command: 
 C:\Program Files (x86)\Code_Saturne\5.0\libexec\code_saturne\cs_solver.exe --param Auto_CFL5_Fo5_0.00001.xml --mpi

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

                                  (R)
                      Code_Saturne

                      Version 5.0.1


  Copyright (C) 1998-2017 EDF S.A., France

  revision 5.0.1
  build 06/14/17 19:39:08
  MPI version 2.0 (MS-MPI)


  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:                07/03/17 15:37:48
  Processor:           
  Directory:           D:\jian.xing\Desktop\Buse\Buse\RESU\Auto_CFL1_Fo1_V
  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:
    SCOTCH 6.0.0

 Reading metadata from file: "mesh_input"

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

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


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




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


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

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

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


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

 --- Physics
       NVAR   =              7 (Nb variables                )
       NSCAL  =              1 (Nb scalars                  )
       NSCAUS =              0 (Nb user scalars             )
       NSCAPP =              1 (Nb specific physics scalars )


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


 ** VOF METHOD                              
    ----------------------------------------

       IVOFMT =             -1 ( -1: inactive                )
                               (  0: active                  )


 ** HOMOGENEOUS MIXTURE MODEL FOR CAVITATION
    ----------------------------------------

       ICAVIT =             -1 (-1: single phase flow       )
                               ( 0: no vap./cond. model     )
                               ( 1: Merkle's model        )


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


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

 --- Per-variable properties

------------------------------------
 Variable          ISTAT      CDTVAR
------------------------------------
 Velocity              1  0.1000E+01
 Pressure              0  0.1000E+01
 k                     1  0.1000E+01
 omega                 1  0.1000E+01
 TempK                 1  0.1000E+01
----------------------------

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

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

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


 ** STOKES
    ------

  -- Phase continue :

       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                   )


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


 ** WALL DISTANCE COMPUTATION
    -------------------------

       ICDPAR =              1 ( 1: std, reread if restart
                               (-1: std, recomputed if restrt
                               ( 2: old, reread if restart
                               (-2: old, recomputed if restrt


       NITMAY =          10000 (Nb iter for iter resolution )
       NSWRSY =              1 (Nb iter for rhs reconstr.   )
       NSWRGY =            100 (Nb iter for grad. reconstr. )
       IMLIGY =              1 (Gradient limitation method  )
       IRCFLY =              1 (Conv. Diff. flow reconstr.  )
       ISCHCY =              1 (Convective scheme           )
       ISSTPY =              0 (Slope tet use               )
       IWARNY =              0 (Verbosity level             )
       NTCMXY =           1000 (Nb iter for steady convect. )

       BLENCY =    0.00000E+00 (2nd order conv. scheme prop.)
       EPSILY =    0.10000E-07 (Iterative solver precision  )
       EPSRSY =    0.10000E-04 (rhs reconstruction precision)
       EPSRGY =    0.10000E-04 (Gradient reconstr. precision)
       CLIMGY =    0.15000E+01 (Coeff. for grad. limitation )
       EXTRAY =    0.00000E+00 (Coeff. for grad. extrapolat.)
       COUMXY =    0.50000E+04 (Max CFL for convection      )
       EPSCVY =    0.10000E-07 (Precision for steady conv.  )
       YPLMXY =    0.20000E+03 (y+ max w. damping influence )


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


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

------------------------------------
 Variable              EPSILO IDIRCL
------------------------------------
 Velocity          0.1000E-04      1
 Pressure          0.1000E-04      1
 k                 0.1000E-04      1
 omega             0.1000E-04      1
 TempK             0.1000E-04      1
------------------------------------

       EPSILO =                (resolution precision)
       IDIRCL = 0 ou 1         (shift diagonal if
                                ISTAT=0 and no Dirichlet)


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


 ** SCALARS
    -------

       ITBRRB =              0 (T or H reconstruction at bdy)

-------------------------------------------------------------
 Variable         Number ISCACP  ITURT     VISLS0      SIGMAS
-------------------------------------------------------------
 TempK                 1      1      0  0.3091E-01  0.1000E+01
-------------------------------------------------------------

------------------------------------
 Variable         Number      RVARFL
------------------------------------
 TempK                 1  0.8000E+00
-------------------------------------------

-------------------------------------------------------
 Variable         Number ICLVFL      SCAMIN      SCAMAX
-------------------------------------------------------
 TempK                 1     -1  0.0000E+00  0.1000E+13
-------------------------------------------------------

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

       For each scalar, the number indicates it's rank
         in the list of all scalars. User scalars are placed
         first, from 1 to NSCAUS. Specific physics scalars
         are placed at the end, from
         NSCAUS+1 to NSCAPP+NSCAUS=NSCAL.

       ISCACP = 0 or 1     2   (use Cp or not               )
       VISLS0 = >0             (Reference viscosity         )
       SIGMAS = >0             (Schmidt                     )
       RVARFL = >0             (Rf, cf variance dissipation )
       ICLVFL = 0, 1 or 2      (Variance clipping mode      )
       SCAMIN =                (Min authorized value        )
       SCAMAX =                (Max authorized value        )
        For variances, SCAMIN is ignored and SCAMAX is used
          only if ICLVFL = 2

------------------------------------------------------
   Scalar        THETSS    IVSEXT      THETVS
------------------------------------------------------
          1  0.0000E+00         0  0.0000E+00
------------------------------------------------------

       THETSS =                (theta for source terms      )
                               ((1+theta).new-theta.old     )
       IVSEXT =                (extrap. total viscosity     )
                               (0: explicit                 )
                               (1: n+thetvs with thetvs=1/2 )
                               (2: n+thetvs with thetvs=1   )
       THETVS =                (theta for scalar diffusivity
                               ((1+theta).new-theta.old     )


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


 ** 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 =          10000 (Final time step required    )

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


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


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

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

 --- Probe history files
       NTHIST =              1 (Output frequency     )
       FRHIST =     -.10000E+01 (Output frequency (s) )
         --           --                --

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

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

 Velocity                       0
 Pressure                       0
 k                              0
 omega                          0
 TempK                          0
 TempK                       -999
 TurbVisc                    -999
 CourantNb                   -999
 FourierNb                   -999
 total_pressure              -999
 Local Time Step             -999
 Yplus                       -999
 M_Pressure                  -999
 M_TemK                      -999
 M_V                         -999
 M_Vx                        -999
 M_Vy                        -999
 M_Vz                        -999
         --           --                --

 --- Additional post-processing variables (ipstdv)
       ipstfo =              0 (Force exerted by the
                                     fluid on the boundary)
       ipstyp =              1 (y+ at boundary)
       ipsttp =              0 (T+ at boundary)
       ipstft =              1 (Thermal flux   at boundary)
       ipstnu =              1 (Dimensionless thermal
                                          flux at boundary)


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


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

       IALE   =              0 (1: activated                )
       NALINF =              0 (Fluid initialization
                                                  iterations)
       IFLXMW =              0 (ALE mass flux computation
                                0: thanks to vertices
                                1: thanks to mesh velocity)


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


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

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

  -5: name: 
      directory: monitoring
      format: time_plot
      options: 
      time dependency: fixed mesh
      output: every 1 time steps

  -6: name: 
      directory: profiles
      format: plot
      options: 
      time dependency: fixed mesh
      output: at calculation end


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

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

 Partitioning by space-filling curve: Morton (in bounding box).
  Number of cells per domain (histogramm):
    [     605504 ;     605505 ] =          4

 Partitioning finished (21.9 s)


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

  Periodicity type: translation
  Transformation matrix:             1            0            0         0.09
                                     0            1            0            0
                                     0            0            1            0

  Selection criteria: "Symmetry_1 or Symmetry_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:          2422019
     Number of interior faces: 5433065
     Number of boundary faces: 137680
     Number of vertices:       937952

  Global number of boundary faces selected for joining:      17302

  Global number of single vertices found:     20
  Global number of single edges found:        20

  Element selection successfully done.
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:       270970
    Vertex-Vertex intersections:          251119
    Other intersections:                   19851

  Joining operation is non-conforming.

  Global number of new vertices to create:       9882

  Equivalences broken for 0 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 26387 global element couples.

  Max size of a merge set of vertices: 4

  Excessive transitivity for 1692 set(s) of vertices.

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

  Edge removed for 0 faces (global).
  Join mesh cleaning done.

  Edge removed for 0 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

  Global number of faces after splitting:      27654

  Global configuration after the joining operation:
     Global number of border faces to add:       3393

  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:          2422019
     Number of interior faces: 5446983
     Number of boundary faces: 123771
     Number of vertices:       937961


  Joining  1 completed (0.967 s).

  All joining operations successfully finished:

    Wall clock time:                 0.967


 ----------------------------------------------------------
 Composing periodicities

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

 Face interfaces creation
 Definition of periodic vertices
 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 =             605504
    maximum value =             605505

      1 : [     605504 ;     605505 ] =          4

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

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

    minimum value =             660796
    maximum value =             666115

      1 : [     660796 ;     661859 [ =          1
      2 : [     661859 ;     662923 [ =          1
      3 : [     662923 ;     663987 [ =          0
      4 : [     663987 ;     665051 [ =          1
      5 : [     665051 ;     666115 ] =          1

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

 Histogram of the number of ghost cells per rank:

    minimum value =              55291
    maximum value =              60610

      1 : [      55291 ;      56354 [ =          1
      2 : [      56354 ;      57418 [ =          1
      3 : [      57418 ;      58482 [ =          0
      4 : [      58482 ;      59546 [ =          1
      5 : [      59546 ;      60610 ] =          1

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

    minimum value =              17726
    maximum value =              20192

      1 : [      17726 ;      18219 [ =          1
      2 : [      18219 ;      18712 [ =          1
      3 : [      18712 ;      19205 [ =          0
      4 : [      19205 ;      19698 [ =          1
      5 : [      19698 ;      20192 ] =          1

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

 Histogram of the number of interior faces per rank:

    minimum value =            1367541
    maximum value =            1370470

      1 : [    1367541 ;    1368126 [ =          2
      2 : [    1368126 ;    1368712 [ =          0
      3 : [    1368712 ;    1369298 [ =          0
      4 : [    1369298 ;    1369884 [ =          1
      5 : [    1369884 ;    1370470 ] =          1

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

 Histogram of the number of boundary faces per rank:

    minimum value =              30754
    maximum value =              31121

      1 : [      30754 ;      30827 [ =          2
      2 : [      30827 ;      30900 [ =          0
      3 : [      30900 ;      30974 [ =          0
      4 : [      30974 ;      31047 [ =          0
      5 : [      31047 ;      31121 ] =          2

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

 Histogram of the number of interior faces per cell:

    minimum value =                  3
    maximum value =                  6

      1 : [          3 ;          4 [ =       9538
      2 : [          4 ;          5 [ =    1450731
      3 : [          5 ;          6 ] =     961750

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

 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

 Start unwarping algorithm


  Histogram of the boundary faces warping before unwarping algorithm:

    minimum value =         0.00000e+000
    maximum value =         1.84741e-013

      1 : [ 0.00000e+000 ; 1.84741e-014 [ =     123767
      2 : [ 1.84741e-014 ; 3.69482e-014 [ =          0
      3 : [ 3.69482e-014 ; 5.54223e-014 [ =          0
      4 : [ 5.54223e-014 ; 7.38964e-014 [ =          0
      5 : [ 7.38964e-014 ; 9.23706e-014 [ =          0
      6 : [ 9.23706e-014 ; 1.10845e-013 [ =          0
      7 : [ 1.10845e-013 ; 1.29319e-013 [ =          0
      8 : [ 1.29319e-013 ; 1.47793e-013 [ =          0
      9 : [ 1.47793e-013 ; 1.66267e-013 [ =          0
     10 : [ 1.66267e-013 ; 1.84741e-013 ] =          4

  Histogram of the interior faces warping before unwarping algorithm:

    minimum value =         0.00000e+000
    maximum value =         4.07659e+001

      1 : [ 0.00000e+000 ; 5.09573e+000 [ =    5248634
      2 : [ 5.09573e+000 ; 1.01915e+001 [ =     116192
      3 : [ 1.01915e+001 ; 1.52872e+001 [ =      57255
      4 : [ 1.52872e+001 ; 2.03829e+001 [ =      16239
      5 : [ 2.03829e+001 ; 2.54787e+001 [ =       1513
      6 : [ 2.54787e+001 ; 3.05744e+001 [ =        151
      7 : [ 3.05744e+001 ; 3.56701e+001 [ =         21
      8 : [ 3.56701e+001 ; 4.07659e+001 ] =         19

Unwarping algorithm converged at iteration 51 

  Histogram of the boundary faces warping after unwarping algorithm:

    minimum value =         0.00000e+000
    maximum value =         5.31088e+000

      1 : [ 0.00000e+000 ; 1.84741e-014 [ =     121493
      2 : [ 1.84741e-014 ; 3.69482e-014 [ =          0
      3 : [ 3.69482e-014 ; 5.54223e-014 [ =          0
      4 : [ 5.54223e-014 ; 7.38964e-014 [ =          0
      5 : [ 7.38964e-014 ; 9.23706e-014 [ =          0
      6 : [ 9.23706e-014 ; 1.10845e-013 [ =          0
      7 : [ 1.10845e-013 ; 1.29319e-013 [ =          0
      8 : [ 1.29319e-013 ; 1.47793e-013 [ =          0
      9 : [ 1.47793e-013 ; 1.66267e-013 [ =          0
     10 : [ 1.66267e-013 ; 1.84741e-013 ] =       2278

  Histogram of the interior faces warping after unwarping algorithm:

    minimum value =         0.00000e+000
    maximum value =         4.08958e+001

      1 : [ 0.00000e+000 ; 5.09573e+000 [ =    5248141
      2 : [ 5.09573e+000 ; 1.01915e+001 [ =     117853
      3 : [ 1.01915e+001 ; 1.52872e+001 [ =      57069
      4 : [ 1.52872e+001 ; 2.03829e+001 [ =      15366
      5 : [ 2.03829e+001 ; 2.54787e+001 [ =       1411
      6 : [ 2.54787e+001 ; 3.05744e+001 [ =        147
      7 : [ 3.05744e+001 ; 3.56701e+001 [ =         19
      8 : [ 3.56701e+001 ; 4.07659e+001 ] =         18

 End unwarping algorithm


 Writing file:        mesh_output
 Finished writing:    mesh_output

 Renumbering mesh:

   renumbering for cells:
     pre-numbering:                       none
     cells adjacent to ghost cells last:  no
     numbering:                           none

   renumbering for interior faces:
     cell adjacency pre-ordering:         lowest id first
     faces adjacent to ghost cells last:  no
     numbering:                           none

   renumbering for boundary faces:
     numbering:                           none

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

 Histogram of volume mesh matrix bandwidth per rank:

    minimum value =             625959
    maximum value =             657347

      1 : [     625959 ;     632236 [ =          1
      2 : [     632236 ;     638514 [ =          0
      3 : [     638514 ;     644791 [ =          1
      4 : [     644791 ;     651069 [ =          0
      5 : [     651069 ;     657347 ] =          2

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =                723
    maximum value =               6915

      1 : [        723 ;       1961 [ =          1
      2 : [       1961 ;       3199 [ =          0
      3 : [       3199 ;       4438 [ =          0
      4 : [       4438 ;       5676 [ =          0
      5 : [       5676 ;       6915 ] =          3

 Mesh coordinates:               minimum    and maximum
                       X : -4.5000018e-002 4.5000004e-002
                       Y : -3.3500074e-001 3.3500076e-001
                       Z : -4.5058969e-033 4.4650140e-002
 Mesh
     Number of cells:          2422019
     Number of interior faces: 5446983
     Number of boundary faces: 123771
     Number of vertices:       937961

 Periodic faces (which are also interior faces):
     Periodicity  1:          6959 face couples

 Groups:
    "Inlet"
       boundary faces:        12644
    "Nappe"
       boundary faces:        26800
    "Outlet"
       boundary faces:         6290
    "Symmetry_1"
       interior faces:         6959
       boundary faces:         1692
    "Symmetry_2"
       interior faces:         6959
       boundary faces:         1701
    "Wall"
       boundary faces:        74644

 --- Information on the volumes
       Minimum control volume      = 2.8229987e-013
       Maximum control volume      = 4.1034232e-008
       Total volume for the domain = 2.5506027e-003

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

  Criterion 2: Offset:
    Number of bad cells detected: 94616 -->   4 %

  Criterion 3: Least-Squares Gradient Quality:
    Number of bad cells detected: 3652 -->   0 %

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

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

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

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

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

 Computing geometric quantities (1.86 s)

 Probe set: "probes":
   maximum distance between cell centers and requested coordinates: 8.262e-007
                                                             
       ALMAX  =    0.13663E+00 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.

       ALMAX is the length used to initialize the turbulence.

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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Pressure          0.0000E+00  0.0000E+00
  k                 0.6000E-03  0.6000E-03
  omega             0.1793E+00  0.1793E+00
  TempK             0.2981E+03  0.2981E+03
 ---------------------------------

                dt  0.1000E-04  0.1000E-04
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.100000000E-04   TIME STEP NUMBER               1
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.9726E+00  0.9726E+00
  molecular_viscos  0.2126E-04  0.2126E-04
  turbulent_viscos  0.3255E-02  0.3255E-02
 -----------------------------------------

 --- Diffusivity:
 -----------------------------------------------
 Scalar           Number  Min. value  Max. value
 -----------------------------------------------
 TempK                 1  0.3091E-01  0.3091E-01
 -----------------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2       12644
Smooth wall               5      101444
Rough wall                6           0
Symmetry                  4        3393
Free outlet               3        6290
Free inlet               14           0
Convective inlet         16           0
Free surface             15           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.42254E-03  -0.33500E+00   0.15686E-04



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644         0.000000000E+00
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.000000000E+00
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.00000E+00 0.00000E+00
   Friction velocity        uk    :  0.29450E-03 0.53755E-03
   Dimensionless distance   yplus :  0.63737E-04 0.38783E-03
   Friction thermal sca.    tstar :  0.00000E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45152E-04 0.27474E-03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


                                                             
 ** WALL DISTANCE                                            
    -------------                                            
                                                             
  Min distance =    0.14899E-04 Max distance =    0.19232E-01
                                                             
     (Distance calculation done in        283 iterations)


   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.41190E-02      33   0.16434E-01   0.20424E+07 0.98132E+05 
c  Velocity[X]                                      0.12851E+06 
c  Velocity[Y]                                      0.14600E+07 
c  Velocity[Z]                                      0.45385E+06 
c  Pressure     0.87483E-03      55   0.40813E+00   0.99828E+00 0.21401E+06 
c  k            0.24032E-03      30   0.12549E-02   0.17100E-02 0.44911E+05 
c  omega        0.10824E+09     101   0.23801E-02   0.15376E+23 0.10000E+07 
c  TempK        0.11886E+06       5   0.16869E-04   0.25654E+05 0.16351E+03 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      8.338e-009                        925114


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -30.533          28.649       -0.005315     -0.00019972
v  Velocity[Y]             -31.306          32.584       0.0048802     -0.00053056
v  Velocity[Z]             -83.181          6.5851        -0.80544        -0.52439
v  ǁVelocityǁ         0.00078794           83.25          3.0008          3.8716
v  Pressure                 30.355     1.3164e+005           79436           80216
v  k                   6.5915e-005       0.0076725      0.00056633      0.00060709
v  omega                   0.17928     7.6639e+010     1.8044e+008     1.0166e+007
v  TempK                    298.15           332.1          298.17           298.2
v  TurbVisc              0.0032549       0.0032549       0.0032549       0.0032549
v  CourantNb                     0               0               0               0
v  FourierNb              0.021072          119.93          1.6913         0.30858
v  total_pressure      1.0136e+005     2.3296e+005     1.8076e+005     1.8154e+005
v  Local Time Step          1e-006        1.1e-005     6.1571e-006     1.0523e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          298.15          298.15          298.15
v  Yplus               0      0.00038783      0.00030165      0.00032539


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.021072          119.93          1.6913         0.30858


 INSTANT    0.200000000E-04   TIME STEP NUMBER               2
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924135E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.33139E-01 0.63151E+01
   Friction velocity        uk    :  0.33112E-01 0.63141E+01
   Dimensionless distance   yplus :  0.23759E-01 0.26410E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.15835E+01
   Rough dim-less th. sca.  tplus :  0.16831E-01 0.18709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.14305E+01      10   0.39844E-05   0.19569E+04 0.48688E+04 
c  Velocity[X]                                      0.52219E+03 
c  Velocity[Y]                                      0.25113E+03 
c  Velocity[Z]                                      0.11835E+04 
c  Pressure     0.47529E-03      40   0.24493E-01   0.88681E+00 0.19923E+06 
c  k            0.22000E-03       5   0.49731E-05   0.33801E-02 0.88287E+05 
c  omega        0.11207E+11       3   0.18161E-06   0.34690E+22 0.90241E+06 
c  TempK        0.10799E+06       3   0.59593E-07   0.16242E+04 0.39434E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -27.524          24.802      -0.0054027     -0.00047478
v  Velocity[Y]             -28.945          28.981       0.0048181     -0.00026273
v  Velocity[Z]             -78.061          6.9546        -0.81323        -0.52073
v  ǁVelocityǁ         0.00098933          78.133          3.0313          3.8878
v  Pressure                  -3064            2598          452.85          481.97
v  k                   9.4621e-009       0.0084328      0.00045127       0.0006011
v  omega                   0.12277     3.8323e+010     9.0993e+007     5.1431e+006
v  TempK                    298.15          335.25          298.18          298.21
v  TurbVisc            9.1438e-016      0.00063533     1.6877e-006     5.6748e-006
v  CourantNb           1.0143e-006               1        0.067621        0.061316
v  FourierNb            0.00028427         0.85615        0.012237       0.0024885
v  total_pressure            98261     1.0392e+005     1.0178e+005     1.0181e+005
v  Local Time Step        1.1e-006       1.21e-005     6.7683e-006     1.1575e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15           332.1          298.53          298.75
v  Yplus               0           2.641         0.56369         0.45063


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0011836          1.5417        0.079858        0.063805


 INSTANT    0.300000000E-04   TIME STEP NUMBER               3
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925145E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.34289E-01 0.55473E+01
   Friction velocity        uk    :  0.34288E-01 0.55473E+01
   Dimensionless distance   yplus :  0.19676E-01 0.28362E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.18545E+01
   Rough dim-less th. sca.  tplus :  0.13939E-01 0.20092E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.13137E+01       9   0.49008E-05   0.93944E+03 0.34632E+04 
c  Velocity[X]                                      0.28048E+03 
c  Velocity[Y]                                      0.12227E+03 
c  Velocity[Z]                                      0.53668E+03 
c  Pressure     0.46179E-03      39   0.14860E-01   0.93379E+00 0.74609E+06 
c  k            0.20012E-03       6   0.46092E-05   0.21429E-03 0.16960E+05 
c  omega        0.28282E+10       3   0.28658E-06   0.78918E+21 0.81512E+06 
c  TempK        0.98192E+05       3   0.75445E-07   0.16789E+04 0.38254E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -8.4195e-009                             3
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -25.734          23.039      -0.0053249     -0.00055377
v  Velocity[Y]             -26.567          26.514       0.0047529     -0.00016915
v  Velocity[Z]             -75.135          6.9097        -0.81691        -0.51913
v  ǁVelocityǁ         0.00037458          75.313          3.0393          3.8889
v  Pressure                -3666.4          1782.1          43.325          71.209
v  k                    2.159e-012         0.00919      0.00043401      0.00060287
v  omega                  0.088655     1.9165e+010     4.6184e+007     2.6245e+006
v  TempK                    298.15          338.31          298.18          298.23
v  TurbVisc            2.4013e-019      0.00074041     1.6393e-006      5.617e-006
v  CourantNb            6.768e-007               1        0.074164        0.067433
v  FourierNb            0.00031243         0.94177        0.013453       0.0027301
v  total_pressure            97659     1.0311e+005     1.0137e+005      1.014e+005
v  Local Time Step       1.21e-006      1.331e-005     7.4433e-006     1.2732e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          335.25          298.62          298.91
v  Yplus               0          2.8362         0.55238         0.44121


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0013059          1.5564        0.087617        0.070163


 INSTANT    0.400000000E-04   TIME STEP NUMBER               4
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924875E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.26113E-01 0.53341E+01
   Friction velocity        uk    :  0.26113E-01 0.53341E+01
   Dimensionless distance   yplus :  0.14985E-01 0.29460E+01
   Friction thermal sca.    tstar : -0.10948E-11 0.22106E+01
   Rough dim-less th. sca.  tplus :  0.10615E-01 0.20870E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.11910E+01       9   0.36895E-05   0.55851E+03 0.27262E+04 
c  Velocity[X]                                      0.17426E+03 
c  Velocity[Y]                                      0.83681E+02 
c  Velocity[Z]                                      0.30057E+03 
c  Pressure     0.37160E-03      29   0.49360E-02   0.77640E+00 0.51179E+05 
c  k            0.18622E-03       6   0.54212E-05   0.12378E-03 0.91067E+04 
c  omega        0.72001E+09       3   0.42198E-06   0.17954E+21 0.73158E+06 
c  TempK        0.89281E+05       3   0.94992E-07   0.17320E+04 0.37075E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.1924e-008                            40
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -23.891          21.774      -0.0052704      -0.0006225
v  Velocity[Y]             -24.538          25.502       0.0047148    -7.3121e-005
v  Velocity[Z]             -73.032            6.66        -0.82146        -0.51809
v  ǁVelocityǁ         0.00010442          73.131          3.0456          3.8896
v  Pressure                -3671.6          1623.8          86.122          112.74
v  k                   8.2996e-016       0.0099233      0.00042623      0.00060588
v  omega                  0.049303     9.5863e+009     2.3708e+007     1.3591e+006
v  TempK                    298.15          341.25          298.19          298.25
v  TurbVisc            1.0956e-022      0.00073253     1.6058e-006     5.5388e-006
v  CourantNb           7.9048e-007               1        0.081586        0.074118
v  FourierNb            0.00034342               1        0.014793       0.0029965
v  total_pressure            97653     1.0295e+005     1.0141e+005     1.0144e+005
v  Local Time Step     1.2848e-006     1.4641e-005     8.1849e-006     1.4004e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          338.31          298.72          299.08
v  Yplus               0           2.946         0.53702            0.43


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0014391          1.4813        0.096379        0.077115


 INSTANT    0.500000000E-04   TIME STEP NUMBER               5
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925887E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.21560E-01 0.51664E+01
   Friction velocity        uk    :  0.21560E-01 0.51664E+01
   Dimensionless distance   yplus :  0.12372E-01 0.30361E+01
   Friction thermal sca.    tstar : -0.30937E-11 0.26021E+01
   Rough dim-less th. sca.  tplus :  0.87644E-02 0.21508E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.10838E+01       9   0.34835E-05   0.41755E+03 0.23176E+04 
c  Velocity[X]                                      0.13229E+03 
c  Velocity[Y]                                      0.68477E+02 
c  Velocity[Z]                                      0.21678E+03 
c  Pressure     0.23609E-03      28   0.29442E-02   0.50129E+00 0.29691E+05 
c  k            0.17447E-03       6   0.64881E-05   0.10661E-03 0.64051E+04 
c  omega        0.18686E+09       3   0.69142E-06   0.40750E+20 0.64693E+06 
c  TempK        0.81181E+05       3   0.12180E-06   0.17848E+04 0.35914E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -5.1951e-008                           177
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.585          20.662      -0.0052256     -0.00069336
v  Velocity[Y]             -22.829          24.126       0.0047245     4.7764e-005
v  Velocity[Z]              -70.55          6.2829        -0.82707        -0.51767
v  ǁVelocityǁ         0.00016269          70.601           3.053          3.8907
v  Pressure                -3580.4          1449.1          117.87          144.77
v  k                   1.9135e-019        0.010626      0.00042154      0.00060961
v  omega                  0.017173     4.7989e+009     1.2416e+007     7.2171e+005
v  TempK                    298.15          344.05           298.2          298.27
v  TurbVisc            8.4979e-026      0.00089849     1.5867e-006     5.4995e-006
v  CourantNb           9.2866e-007               1        0.089623        0.081455
v  FourierNb            0.00037753               1        0.016267       0.0032917
v  total_pressure            97745     1.0277e+005     1.0144e+005     1.0147e+005
v  Local Time Step     1.2848e-006     1.6105e-005     8.9993e-006     1.5403e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          341.25          298.81          299.26
v  Yplus               0          3.0361         0.52089         0.41834


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0015856          1.3581         0.10589        0.084747


 INSTANT    0.600000000E-04   TIME STEP NUMBER               6
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925630E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.19080E-01 0.51399E+01
   Friction velocity        uk    :  0.19080E-01 0.51399E+01
   Dimensionless distance   yplus :  0.10949E-01 0.31180E+01
   Friction thermal sca.    tstar : -0.75275E-11 0.30220E+01
   Rough dim-less th. sca.  tplus :  0.77562E-02 0.22088E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.98665E+00       9   0.35196E-05   0.34707E+03 0.20449E+04 
c  Velocity[X]                                      0.11159E+03 
c  Velocity[Y]                                      0.59025E+02 
c  Velocity[Z]                                      0.17646E+03 
c  Pressure     0.80302E-04      25   0.24251E-02   0.17190E+00 0.98899E+04 
c  k            0.16441E-03       7   0.62998E-05   0.10194E-03 0.50555E+04 
c  omega        0.50776E+08       3   0.11750E-05   0.91300E+19 0.55059E+06 
c  TempK        0.73817E+05       3   0.15741E-06   0.18372E+04 0.34771E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -7.3492e-008                           436
a  omega                  -0.18966                             6
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -21.835          19.824      -0.0052215     -0.00075504
v  Velocity[Y]             -22.108          23.457       0.0047924      0.00022682
v  Velocity[Z]             -67.914          5.8798        -0.83292        -0.51753
v  ǁVelocityǁ         0.00021186          67.939          3.0616          3.8924
v  Pressure                -3452.1          1278.4           109.6           135.8
v  k                   2.6779e-023        0.011289      0.00041845      0.00061397
v  omega                 0.0012669      2.409e+009     6.7456e+006     4.0012e+005
v  TempK                    298.15          346.67          298.21          298.29
v  TurbVisc            5.2043e-029      0.00082457     1.5656e-006     5.4326e-006
v  CourantNb           1.0387e-006               1        0.098329        0.089504
v  FourierNb            0.00041514               1        0.017887       0.0036149
v  total_pressure            97873      1.026e+005     1.0143e+005     1.0146e+005
v  Local Time Step     1.2848e-006     1.7716e-005     9.8933e-006     1.6942e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          344.05          298.92          299.45
v  Yplus               0           3.118         0.51115         0.40769


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001746          1.3621         0.11622        0.093119


 INSTANT    0.700000000E-04   TIME STEP NUMBER               7
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925797E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18161E-01 0.54008E+01
   Friction velocity        uk    :  0.18161E-01 0.54008E+01
   Dimensionless distance   yplus :  0.10421E-01 0.31930E+01
   Friction thermal sca.    tstar : -0.14924E-10 0.34670E+01
   Rough dim-less th. sca.  tplus :  0.73826E-02 0.22619E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         64 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.89844E+00       9   0.36500E-05   0.30537E+03 0.18318E+04 
c  Velocity[X]                                      0.99081E+02 
c  Velocity[Y]                                      0.51900E+02 
c  Velocity[Z]                                      0.15439E+03 
c  Pressure     0.97809E-04      26   0.27173E-02   0.21047E+00 0.19335E+05 
c  k            0.15577E-03       7   0.72235E-05   0.10113E-03 0.42346E+04 
c  omega        0.15441E+08       4   0.18086E-05   0.19384E+19 0.42241E+06 
c  TempK        0.67123E+05       3   0.20398E-06   0.18891E+04 0.33650E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -5.7091e-008                          3664
a  omega                  -0.21919                            13
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -21.41          18.686      -0.0052098     -0.00079269
v  Velocity[Y]             -21.715           22.96       0.0048902      0.00041527
v  Velocity[Z]             -65.274           7.405        -0.83903         -0.5175
v  ǁVelocityǁ         0.00020809          65.285          3.0707          3.8942
v  Pressure                -3289.3          1121.3          90.891          115.74
v  k                   8.6206e-024        0.011908      0.00041644      0.00061894
v  omega                 0.0084641     1.2217e+009     3.9298e+006     2.3921e+005
v  TempK                    298.15           349.1          298.22          298.32
v  TurbVisc            1.0811e-032       0.0010224     1.5444e-006     5.3781e-006
v  CourantNb           1.1285e-006               1         0.10774        0.098324
v  FourierNb            0.00045659               1        0.019667       0.0039694
v  total_pressure            98036     1.0245e+005     1.0142e+005     1.0144e+005
v  Local Time Step     1.2848e-006     1.9487e-005     1.0874e-005     1.8634e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          346.67          299.02          299.65
v  Yplus               0           3.193         0.50283         0.39711


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0019219          1.3774         0.12741         0.10229


 INSTANT    0.800000000E-04   TIME STEP NUMBER               8
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924983E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18075E-01 0.56062E+01
   Friction velocity        uk    :  0.18075E-01 0.56062E+01
   Dimensionless distance   yplus :  0.10372E-01 0.32591E+01
   Friction thermal sca.    tstar : -0.27742E-10 0.39346E+01
   Rough dim-less th. sca.  tplus :  0.73479E-02 0.23088E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         83 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.81824E+00       9   0.39837E-05   0.28244E+03 0.16761E+04 
c  Velocity[X]                                      0.91917E+02 
c  Velocity[Y]                                      0.47085E+02 
c  Velocity[Z]                                      0.14343E+03 
c  Pressure     0.73708E-04      24   0.20254E-02   0.15925E+00 0.93392E+04 
c  k            0.14831E-03       7   0.81360E-05   0.10192E-03 0.36666E+04 
c  omega        0.60114E+07       4   0.20891E-05   0.34063E+18 0.24899E+06 
c  TempK        0.61038E+05       3   0.26545E-06   0.19408E+04 0.32551E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.0584e-007                          4604
a  omega                  -0.21983                            19
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -20.747          17.876      -0.0051822     -0.00081522
v  Velocity[Y]             -21.363          22.287       0.0050141      0.00057514
v  Velocity[Z]             -62.822          8.3747        -0.84545        -0.51747
v  ǁVelocityǁ         0.00020451          62.896          3.0805          3.8961
v  Pressure                -3123.4          969.88          82.648          106.21
v  k                        1e-024        0.012477      0.00041525      0.00062456
v  omega                   0.00212     6.4313e+008     2.6005e+006     1.6241e+005
v  TempK                    298.15          351.31          298.23          298.34
v  TurbVisc            6.8626e-033      0.00088653     1.5202e-006     5.3047e-006
v  CourantNb           1.2051e-006               1         0.11791         0.10798
v  FourierNb            0.00050221               1        0.021623       0.0043571
v  total_pressure            98202     1.0229e+005     1.0141e+005     1.0143e+005
v  Local Time Step     1.2848e-006     2.1436e-005     1.1949e-005     2.0494e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15           349.1          299.13          299.86
v  Yplus               0          3.2591         0.49383         0.38623


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0021152          1.3127         0.13953         0.11234


 INSTANT    0.900000000E-04   TIME STEP NUMBER               9
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925266E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18216E-01 0.57411E+01
   Friction velocity        uk    :  0.18216E-01 0.57411E+01
   Dimensionless distance   yplus :  0.10453E-01 0.33164E+01
   Friction thermal sca.    tstar : -0.49436E-10 0.44227E+01
   Rough dim-less th. sca.  tplus :  0.74049E-02 0.23494E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         94 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.74544E+00       9   0.44033E-05   0.26952E+03 0.15576E+04 
c  Velocity[X]                                      0.88587E+02 
c  Velocity[Y]                                      0.44054E+02 
c  Velocity[Z]                                      0.13688E+03 
c  Pressure     0.61688E-04      23   0.18438E-02   0.13370E+00 0.50974E+04 
c  k            0.14185E-03       8   0.79816E-05   0.10355E-03 0.32369E+04 
c  omega        0.36836E+07       4   0.13623E-05   0.48796E+17 0.10698E+06 
c  TempK        0.55507E+05       3   0.34651E-06   0.19924E+04 0.31479E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.1688e-007                          4695
a  omega                   -0.2527                            19
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.872          17.097      -0.0051508      -0.0008496
v  Velocity[Y]             -21.381          21.729       0.0051563      0.00072765
v  Velocity[Z]             -61.369           9.085        -0.85212        -0.51735
v  ǁVelocityǁ         0.00020315          61.431           3.091          3.8982
v  Pressure                -2940.6          825.29          78.441          101.12
v  k                    1.061e-024        0.012992      0.00041475      0.00063088
v  omega                 0.0023171     3.8135e+008     2.0198e+006      1.277e+005
v  TempK                    298.15          353.28          298.24          298.37
v  TurbVisc            1.5122e-033       0.0011019     1.4954e-006     5.2323e-006
v  CourantNb           1.2712e-006               1         0.12886         0.11854
v  FourierNb             0.0005524               1         0.02377        0.004782
v  total_pressure            98384     1.0215e+005      1.014e+005     1.0143e+005
v  Local Time Step     1.2848e-006     2.3579e-005     1.3126e-005     2.2538e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          351.31          299.25          300.07
v  Yplus               0          3.3164         0.48434         0.37518


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0023277          1.2817         0.15263         0.12332


 INSTANT    0.100000000E-03   TIME STEP NUMBER              10
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925704E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18356E-01 0.58005E+01
   Friction velocity        uk    :  0.18356E-01 0.58005E+01
   Dimensionless distance   yplus :  0.10534E-01 0.33743E+01
   Friction thermal sca.    tstar : -0.83966E-10 0.49290E+01
   Rough dim-less th. sca.  tplus :  0.74621E-02 0.23904E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         98 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.67938E+00       9   0.49309E-05   0.26255E+03 0.14610E+04 
c  Velocity[X]                                      0.87193E+02 
c  Velocity[Y]                                      0.41691E+02 
c  Velocity[Z]                                      0.13367E+03 
c  Pressure     0.58002E-04      27   0.18330E-02   0.12605E+00 0.39472E+04 
c  k            0.13622E-03       8   0.84323E-05   0.10570E-03 0.28909E+04 
c  omega        0.31559E+07       4   0.78318E-06   0.92322E+16 0.46696E+05 
c  TempK        0.50479E+05       3   0.45478E-06   0.20441E+04 0.30434E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.2857e-007                          4358
a  omega                  -0.43551                            24
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.878          16.628      -0.0051297     -0.00089366
v  Velocity[Y]             -21.132          21.528       0.0053132      0.00087289
v  Velocity[Z]             -59.728          9.5278        -0.85908        -0.51716
v  ǁVelocityǁ         0.00020222          59.778          3.1023          3.9006
v  Pressure                -2749.5          708.81          74.965          97.016
v  k                    3.654e-022        0.013451      0.00041487      0.00063796
v  omega                0.00072236     2.9006e+008     1.7577e+006     1.1089e+005
v  TempK                    298.15          355.03          298.25          298.41
v  TurbVisc            2.7059e-033      0.00096574     1.4714e-006      5.164e-006
v  CourantNb           1.3308e-006               1         0.14067          0.1301
v  FourierNb            0.00060755               1        0.026128       0.0052482
v  total_pressure            98575     1.0203e+005      1.014e+005     1.0142e+005
v  Local Time Step     1.2848e-006     2.5937e-005     1.4416e-005     2.4785e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          353.28          299.37           300.3
v  Yplus               0          3.3743         0.47455         0.36409


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0025616          1.3679          0.1668         0.13535


 INSTANT    0.110000000E-03   TIME STEP NUMBER              11
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925924E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18422E-01 0.57923E+01
   Friction velocity        uk    :  0.18422E-01 0.57922E+01
   Dimensionless distance   yplus :  0.10571E-01 0.34286E+01
   Friction thermal sca.    tstar : -0.13898E-09 0.54601E+01
   Rough dim-less th. sca.  tplus :  0.74888E-02 0.24288E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         97 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.61946E+00      10   0.33007E-05   0.25900E+03 0.13789E+04 
c  Velocity[X]                                      0.86621E+02 
c  Velocity[Y]                                      0.39703E+02 
c  Velocity[Z]                                      0.13267E+03 
c  Pressure     0.54896E-04      26   0.18428E-02   0.11962E+00 0.32523E+04 
c  k            0.13127E-03       8   0.89457E-05   0.10827E-03 0.26004E+04 
c  omega        0.30525E+07       4   0.53164E-06   0.25101E+16 0.23585E+05 
c  TempK        0.45909E+05       3   0.59925E-06   0.20964E+04 0.29418E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.8855e-007                          4001
a  omega                  -0.62311                            27
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.035          16.226       -0.005116     -0.00094868
v  Velocity[Y]             -20.714          21.263       0.0054669       0.0010148
v  Velocity[Z]             -57.939          9.5612        -0.86665          -0.517
v  ǁVelocityǁ         0.00020223          57.977          3.1149          3.9033
v  Pressure                -2555.5          606.66          72.081          93.597
v  k                   9.4996e-021        0.013853      0.00041557      0.00064588
v  omega                 0.0045468     2.7478e+008     1.6158e+006     1.0122e+005
v  TempK                    298.15          356.53          298.26          298.44
v  TurbVisc            2.1317e-030       0.0010027     1.4482e-006     5.1053e-006
v  CourantNb           1.3868e-006               1         0.15342         0.14274
v  FourierNb            0.00066823               1        0.028718       0.0057598
v  total_pressure            98769     1.0193e+005      1.014e+005     1.0142e+005
v  Local Time Step     1.2848e-006     2.8531e-005     1.5827e-005     2.7255e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          355.03          299.49          300.53
v  Yplus               0          3.4286         0.46454         0.35303


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0028194          1.4499         0.18213          0.1485


 INSTANT    0.120000000E-03   TIME STEP NUMBER              12
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925949E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18470E-01 0.58186E+01
   Friction velocity        uk    :  0.18470E-01 0.58185E+01
   Dimensionless distance   yplus :  0.10599E-01 0.34693E+01
   Friction thermal sca.    tstar : -0.22439E-09 0.60074E+01
   Rough dim-less th. sca.  tplus :  0.75083E-02 0.24577E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         65 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.56514E+00      10   0.37187E-05   0.25703E+03 0.13055E+04 
c  Velocity[X]                                      0.86352E+02 
c  Velocity[Y]                                      0.38038E+02 
c  Velocity[Z]                                      0.13265E+03 
c  Pressure     0.54140E-04      26   0.18809E-02   0.11828E+00 0.27056E+04 
c  k            0.12688E-03       8   0.93146E-05   0.11119E-03 0.23495E+04 
c  omega        0.30194E+07       3   0.14070E-05   0.79770E+15 0.12762E+05 
c  TempK        0.41754E+05       3   0.79006E-06   0.21494E+04 0.28434E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.4799e-007                          3611
a  omega                  -0.40439                            27
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -17.134          15.799       -0.005106      -0.0010074
v  Velocity[Y]             -20.934          20.852       0.0056223        0.001184
v  Velocity[Z]             -56.042          10.562          -0.875         -0.5169
v  ǁVelocityǁ         0.00020199          56.072          3.1289          3.9064
v  Pressure                -2373.5          521.37          69.634          90.585
v  k                   1.4252e-020          0.0142      0.00041685      0.00065471
v  omega                0.00042885     2.7408e+008     1.5287e+006           95007
v  TempK                    298.15          357.81          298.28          298.48
v  TurbVisc             5.784e-029      0.00093879     1.4257e-006      5.053e-006
v  CourantNb           1.4366e-006               1         0.16716         0.15656
v  FourierNb              0.000735               1         0.03156        0.006321
v  total_pressure            98951     1.0185e+005     1.0139e+005     1.0142e+005
v  Local Time Step     1.2848e-006     3.1384e-005      1.737e-005     2.9968e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          356.53          299.61          300.77
v  Yplus               0          3.4693         0.45447          0.3421


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0031028          1.5141         0.19872         0.16288


 INSTANT    0.130000000E-03   TIME STEP NUMBER              13
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925873E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18479E-01 0.58393E+01
   Friction velocity        uk    :  0.18479E-01 0.58391E+01
   Dimensionless distance   yplus :  0.10604E-01 0.34975E+01
   Friction thermal sca.    tstar : -0.35386E-09 0.65671E+01
   Rough dim-less th. sca.  tplus :  0.75122E-02 0.24777E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         95 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.51593E+00      10   0.41902E-05   0.25571E+03 0.12387E+04 
c  Velocity[X]                                      0.86493E+02 
c  Velocity[Y]                                      0.36704E+02 
c  Velocity[Z]                                      0.13251E+03 
c  Pressure     0.57518E-04      23   0.18467E-02   0.12597E+00 0.27718E+04 
c  k            0.12294E-03       8   0.90986E-05   0.11442E-03 0.21287E+04 
c  omega        0.29962E+07       3   0.12344E-05   0.29092E+15 0.73728E+04 
c  TempK        0.37979E+05       3   0.10403E-05   0.22036E+04 0.27483E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -4.27e-007                          3020
a  omega                  -0.70059                            28
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -16.127          15.355      -0.0050779      -0.0010711
v  Velocity[Y]             -21.151          20.805       0.0057856       0.0013832
v  Velocity[Z]             -54.082          11.145        -0.88414        -0.51683
v  ǁVelocityǁ         0.00020011          54.107          3.1446            3.91
v  Pressure                -2245.4          447.56          66.522           86.89
v  k                   2.3418e-019        0.014535      0.00041868      0.00066456
v  omega                 0.0050567     2.7402e+008     1.4718e+006           90769
v  TempK                    298.15          358.87          298.29          298.52
v  TurbVisc            1.9821e-028      0.00072871      1.402e-006     4.9933e-006
v  CourantNb           1.4831e-006               1         0.18198         0.17166
v  FourierNb            0.00080844               1        0.034681        0.006935
v  total_pressure            99080     1.0177e+005     1.0139e+005     1.0141e+005
v  Local Time Step     1.2848e-006     3.4523e-005     1.9057e-005     3.2948e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          357.81          299.74          301.01
v  Yplus               0          3.4975         0.44449          0.3314


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0034146          1.5501         0.21666          0.1786


 INSTANT    0.140000000E-03   TIME STEP NUMBER              14
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925367E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18416E-01 0.58315E+01
   Friction velocity        uk    :  0.18416E-01 0.58314E+01
   Dimensionless distance   yplus :  0.10568E-01 0.35120E+01
   Friction thermal sca.    tstar : -0.54592E-09 0.71365E+01
   Rough dim-less th. sca.  tplus :  0.74863E-02 0.24879E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        123 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.47138E+00      10   0.47058E-05   0.25437E+03 0.11760E+04 
c  Velocity[X]                                      0.87253E+02 
c  Velocity[Y]                                      0.35596E+02 
c  Velocity[Z]                                      0.13152E+03 
c  Pressure     0.59060E-04      27   0.18939E-02   0.12962E+00 0.26874E+04 
c  k            0.11935E-03       9   0.83853E-05   0.11796E-03 0.19323E+04 
c  omega        0.29760E+07       3   0.10945E-05   0.12313E+15 0.45816E+04 
c  TempK        0.34548E+05       3   0.13721E-05   0.22593E+04 0.26564E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -8.0996e-007                          2343
a  omega                   -0.4256                            27
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -15.342          14.908      -0.0050289      -0.0011322
v  Velocity[Y]             -21.681          21.154       0.0059435       0.0016036
v  Velocity[Z]             -52.097          11.542        -0.89403         -0.5167
v  ǁVelocityǁ           0.000197          52.119          3.1622          3.9142
v  Pressure                  -2168           399.6          63.129          82.933
v  k                   8.6546e-019        0.014834      0.00042108      0.00067552
v  omega                 0.0058856     2.7401e+008     1.4327e+006           87740
v  TempK                    298.15          359.73          298.31          298.57
v  TurbVisc            1.2465e-027      0.00058889     1.3765e-006     4.9266e-006
v  CourantNb           1.5287e-006               1         0.19792         0.18814
v  FourierNb            0.00088921               1        0.038103       0.0076062
v  total_pressure            99157     1.0172e+005     1.0139e+005     1.0141e+005
v  Local Time Step     1.2848e-006     3.7975e-005     2.0898e-005     3.6221e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          358.87          299.87          301.26
v  Yplus               0           3.512         0.43459         0.32096


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0037579          1.5651         0.23603         0.19575


 INSTANT    0.150000000E-03   TIME STEP NUMBER              15
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925810E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18290E-01 0.58751E+01
   Friction velocity        uk    :  0.18290E-01 0.58748E+01
   Dimensionless distance   yplus :  0.10496E-01 0.35126E+01
   Friction thermal sca.    tstar : -0.82274E-09 0.77122E+01
   Rough dim-less th. sca.  tplus :  0.74353E-02 0.24883E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        156 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.43108E+00      10   0.52461E-05   0.25227E+03 0.11163E+04 
c  Velocity[X]                                      0.87837E+02 
c  Velocity[Y]                                      0.34397E+02 
c  Velocity[Z]                                      0.13003E+03 
c  Pressure     0.68026E-04      28   0.18944E-02   0.14963E+00 0.29781E+04 
c  k            0.11605E-03       9   0.90096E-05   0.12179E-03 0.17562E+04 
c  omega        0.29578E+07       3   0.97510E-06   0.59594E+14 0.30423E+04 
c  TempK        0.31429E+05       4   0.37005E-06   0.23207E+04 0.25700E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.0274e-006                          1676
a  omega                  -0.75615                            28
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -14.739          14.471      -0.0049584      -0.0011935
v  Velocity[Y]             -22.333          21.482       0.0060921       0.0018474
v  Velocity[Z]             -51.036          11.654        -0.90488        -0.51655
v  ǁVelocityǁ         0.00019448          51.045          3.1819          3.9188
v  Pressure                -2112.4          364.46          58.688          78.029
v  k                   1.9319e-018        0.015082      0.00042405       0.0006877
v  omega                0.00085787     2.7401e+008     1.4044e+006           85480
v  TempK                    298.15          360.41          298.33          298.63
v  TurbVisc            5.2826e-027      0.00047396     1.3503e-006     4.8603e-006
v  CourantNb           1.5741e-006               1           0.215         0.20609
v  FourierNb            0.00097807               1        0.041856       0.0083398
v  total_pressure            99213     1.0169e+005     1.0138e+005      1.014e+005
v  Local Time Step     1.2848e-006     4.1772e-005     2.2903e-005     3.9812e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          359.73             300          301.52
v  Yplus               0          3.5126         0.42466         0.31083


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0041357          1.5586         0.25686         0.21443


 INSTANT    0.160000000E-03   TIME STEP NUMBER              16
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925619E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18188E-01 0.59699E+01
   Friction velocity        uk    :  0.18188E-01 0.59696E+01
   Dimensionless distance   yplus :  0.10437E-01 0.34995E+01
   Friction thermal sca.    tstar : -0.11917E-08 0.82946E+01
   Rough dim-less th. sca.  tplus :  0.73936E-02 0.24791E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        140 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.39468E+00      10   0.58355E-05   0.24988E+03 0.10598E+04 
c  Velocity[X]                                      0.87804E+02 
c  Velocity[Y]                                      0.33189E+02 
c  Velocity[Z]                                      0.12889E+03 
c  Pressure     0.74350E-04      28   0.20280E-02   0.16384E+00 0.28831E+04 
c  k            0.11296E-03       9   0.97112E-05   0.12594E-03 0.15980E+04 
c  omega        0.29414E+07       3   0.87147E-06   0.31537E+14 0.21115E+04 
c  TempK        0.28597E+05       4   0.49412E-06   0.23808E+04 0.24848E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.3494e-006                          1352
a  omega                  -0.72487                            35
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -15.34          15.079      -0.0048691      -0.0012613
v  Velocity[Y]             -22.737           21.71       0.0062302       0.0021148
v  Velocity[Z]             -50.034          11.724        -0.91689        -0.51641
v  ǁVelocityǁ         0.00019198          50.036          3.2044           3.924
v  Pressure                -2067.6          336.46          54.016          72.971
v  k                   3.9799e-018        0.015283      0.00042759      0.00070121
v  omega                 0.0014745     2.7401e+008     1.3832e+006           83733
v  TempK                    298.15          360.95          298.34          298.68
v  TurbVisc            4.8909e-026      0.00042266      1.324e-006     4.7983e-006
v  CourantNb           1.6214e-006               1         0.23322          0.2256
v  FourierNb             0.0010758               1        0.045967       0.0091412
v  total_pressure            99257     1.0166e+005     1.0138e+005      1.014e+005
v  Local Time Step     1.2848e-006      4.595e-005     2.5081e-005     4.3751e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          360.41          300.13          301.78
v  Yplus               0          3.4995         0.41499         0.30115


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0045515          1.5391         0.27919         0.23474


 INSTANT    0.170000000E-03   TIME STEP NUMBER              17
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925405E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18085E-01 0.60727E+01
   Friction velocity        uk    :  0.18085E-01 0.60722E+01
   Dimensionless distance   yplus :  0.10378E-01 0.35330E+01
   Friction thermal sca.    tstar : -0.16859E-08 0.88784E+01
   Rough dim-less th. sca.  tplus :  0.73518E-02 0.25028E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        141 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.36186E+00      11   0.47157E-05   0.24748E+03 0.10062E+04 
c  Velocity[X]                                      0.87598E+02 
c  Velocity[Y]                                      0.32142E+02 
c  Velocity[Z]                                      0.12774E+03 
c  Pressure     0.83000E-04      29   0.20574E-02   0.18309E+00 0.28409E+04 
c  k            0.11005E-03       9   0.10376E-04   0.13040E-03 0.14555E+04 
c  omega        0.29265E+07       3   0.78393E-06   0.17761E+14 0.15115E+04 
c  TempK        0.26023E+05       4   0.66893E-06   0.24432E+04 0.24027E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.7215e-006                          1190
a  omega                  -0.73493                            33
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -15.844          15.956      -0.0047631      -0.0013319
v  Velocity[Y]             -22.863          21.786       0.0063593       0.0023956
v  Velocity[Z]             -49.151          11.564        -0.93011        -0.51629
v  ǁVelocityǁ          0.0001882          49.157          3.2297          3.9298
v  Pressure                -2037.4          313.69           49.06          67.669
v  k                    8.843e-019         0.01569      0.00043175      0.00071619
v  omega                 0.0029576     2.7401e+008     1.3666e+006           82344
v  TempK                    298.15          361.46          298.37          298.75
v  TurbVisc            1.0052e-025      0.00040783     1.2972e-006     4.7388e-006
v  CourantNb           1.6698e-006               1         0.25255         0.24674
v  FourierNb             0.0011834               1        0.050467        0.010015
v  total_pressure            99288     1.0164e+005     1.0137e+005     1.0139e+005
v  Local Time Step     1.2848e-006     5.0545e-005     2.7441e-005     4.8066e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          360.95          300.26          302.04
v  Yplus               0           3.533         0.40583         0.29201


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0050088          1.5094         0.30302         0.25676


 INSTANT    0.180000000E-03   TIME STEP NUMBER              18
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925453E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17918E-01 0.61832E+01
   Friction velocity        uk    :  0.17918E-01 0.61827E+01
   Dimensionless distance   yplus :  0.10282E-01 0.35972E+01
   Friction thermal sca.    tstar : -0.23173E-08 0.94620E+01
   Rough dim-less th. sca.  tplus :  0.72839E-02 0.25483E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        137 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.33233E+00      11   0.52013E-05   0.24465E+03 0.95514E+03 
c  Velocity[X]                                      0.87506E+02 
c  Velocity[Y]                                      0.31215E+02 
c  Velocity[Z]                                      0.12593E+03 
c  Pressure     0.10190E-03      28   0.20853E-02   0.22482E+00 0.33148E+04 
c  k            0.10726E-03       9   0.11060E-04   0.13518E-03 0.13272E+04 
c  omega        0.29130E+07       3   0.70777E-06   0.10459E+14 0.11062E+04 
c  TempK        0.23686E+05       4   0.91208E-06   0.25081E+04 0.23236E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.1923e-006                          1099
a  omega                  -0.74859                            30
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -16.271          16.736      -0.0046436       -0.001399
v  Velocity[Y]             -22.874          21.773       0.0064772       0.0026937
v  Velocity[Z]              -48.13          11.553        -0.94452        -0.51614
v  ǁVelocityǁ         0.00018558          48.148          3.2582          3.9363
v  Pressure                  -1999          289.59           42.84          61.132
v  k                    1.276e-016        0.016031      0.00043657      0.00073276
v  omega                 0.0013241     2.7401e+008     1.3534e+006           81216
v  TempK                    298.15          361.88          298.39          298.82
v  TurbVisc             2.213e-026      0.00038694     1.2706e-006     4.6832e-006
v  CourantNb           1.7235e-006               1         0.27299         0.26959
v  FourierNb             0.0013017               1        0.055388        0.010967
v  total_pressure            99326     1.0161e+005     1.0137e+005     1.0139e+005
v  Local Time Step     1.2848e-006     5.5599e-005     2.9988e-005     5.2788e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          361.46           300.4           302.3
v  Yplus               0          3.5972         0.39754         0.28353


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0055118          1.5491         0.32838         0.28056


 INSTANT    0.190000000E-03   TIME STEP NUMBER              19
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925236E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17801E-01 0.62945E+01
   Friction velocity        uk    :  0.17801E-01 0.62939E+01
   Dimensionless distance   yplus :  0.10215E-01 0.36619E+01
   Friction thermal sca.    tstar : -0.30691E-08 0.10044E+02
   Rough dim-less th. sca.  tplus :  0.72366E-02 0.25941E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        152 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.30584E+00      11   0.56979E-05   0.24159E+03 0.90717E+03 
c  Velocity[X]                                      0.87254E+02 
c  Velocity[Y]                                      0.30364E+02 
c  Velocity[Z]                                      0.12397E+03 
c  Pressure     0.11532E-03      29   0.21403E-02   0.25422E+00 0.34696E+04 
c  k            0.10456E-03       9   0.11875E-04   0.14031E-03 0.12118E+04 
c  omega        0.29007E+07       3   0.64295E-06   0.63649E+13 0.82299E+03 
c  TempK        0.21565E+05       4   0.12462E-05   0.25755E+04 0.22472E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.7284e-006                          1014
a  omega                  -0.76639                            29
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -16.564          18.859      -0.0045243      -0.0014714
v  Velocity[Y]             -22.599          21.721       0.0065783       0.0030106
v  Velocity[Z]             -46.929           12.81         -0.9601        -0.51599
v  ǁVelocityǁ         0.00018302          46.964          3.2898          3.9436
v  Pressure                -1967.3          262.11          36.044          54.034
v  k                   4.9981e-016         0.01632      0.00044211      0.00075109
v  omega                 0.0023808       2.74e+008     1.3427e+006           80286
v  TempK                    298.15          362.23          298.41          298.89
v  TurbVisc            3.1837e-024      0.00036249     1.2437e-006     4.6284e-006
v  CourantNb            1.781e-006               1         0.29449         0.29418
v  FourierNb             0.0014318               1        0.060763        0.012001
v  total_pressure            99358     1.0159e+005     1.0136e+005     1.0138e+005
v  Local Time Step     1.2848e-006     6.1159e-005     3.2726e-005     5.7948e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          361.88          300.53          302.57
v  Yplus               0          3.6619         0.39007         0.27571


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0060656          1.7178         0.35525         0.30618


 INSTANT    0.200000000E-03   TIME STEP NUMBER              20
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925323E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17686E-01 0.63982E+01
   Friction velocity        uk    :  0.17686E-01 0.63975E+01
   Dimensionless distance   yplus :  0.10149E-01 0.37222E+01
   Friction thermal sca.    tstar : -0.38650E-08 0.10624E+02
   Rough dim-less th. sca.  tplus :  0.71898E-02 0.26368E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        156 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.28215E+00      11   0.62506E-05   0.23824E+03 0.86247E+03 
c  Velocity[X]                                      0.86997E+02 
c  Velocity[Y]                                      0.29606E+02 
c  Velocity[Z]                                      0.12163E+03 
c  Pressure     0.12574E-03      30   0.21609E-02   0.27665E+00 0.34777E+04 
c  k            0.10194E-03      10   0.12064E-04   0.14584E-03 0.11082E+04 
c  omega        0.28896E+07       3   0.58921E-06   0.39861E+13 0.62113E+03 
c  TempK        0.19641E+05       4   0.17022E-05   0.26456E+04 0.21735E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.8146e-006                           942
a  omega                   -1.0849                            24
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -17.883          21.566      -0.0044075       -0.001558
v  Velocity[Y]              -22.05          21.612       0.0066645       0.0033397
v  Velocity[Z]             -45.855          13.012        -0.97684        -0.51586
v  ǁVelocityǁ         0.00018135           45.95          3.3249          3.9517
v  Pressure                -1978.3          239.03          28.997          46.683
v  k                    7.564e-017        0.016619      0.00044846      0.00077133
v  omega                 0.0041354       2.74e+008     1.3339e+006           79512
v  TempK                    298.15          362.52          298.44          298.98
v  TurbVisc            9.8862e-024      0.00033198     1.2172e-006     4.5751e-006
v  CourantNb           1.8581e-006               1         0.31695         0.32049
v  FourierNb             0.0015748               1        0.066627        0.013122
v  total_pressure            99347     1.0156e+005     1.0135e+005     1.0137e+005
v  Local Time Step     1.2848e-006     6.7275e-005     3.5655e-005     6.3572e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          362.23          300.66          302.83
v  Yplus               0          3.7222         0.38347         0.26858


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0066767          1.8607         0.38357         0.33361


 INSTANT    0.210000000E-03   TIME STEP NUMBER              21
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925481E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17612E-01 0.64836E+01
   Friction velocity        uk    :  0.17612E-01 0.64827E+01
   Dimensionless distance   yplus :  0.10106E-01 0.37718E+01
   Friction thermal sca.    tstar : -0.45054E-08 0.11204E+02
   Rough dim-less th. sca.  tplus :  0.71594E-02 0.26720E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        134 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26108E+00      11   0.68383E-05   0.23490E+03 0.82141E+03 
c  Velocity[X]                                      0.86762E+02 
c  Velocity[Y]                                      0.29007E+02 
c  Velocity[Z]                                      0.11913E+03 
c  Pressure     0.14087E-03      28   0.21294E-02   0.30894E+00 0.36122E+04 
c  k            0.99372E-04      10   0.13231E-04   0.15186E-03 0.10153E+04 
c  omega        0.28794E+07       3   0.54387E-06   0.25594E+13 0.47475E+03 
c  TempK        0.17898E+05       4   0.23187E-05   0.27188E+04 0.21024E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.2258e-006                           872
a  omega                   -1.1234                            22
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.911          24.007      -0.0042898      -0.0016549
v  Velocity[Y]             -21.463          21.393       0.0067563       0.0036867
v  Velocity[Z]             -45.063          13.838        -0.99468        -0.51574
v  ǁVelocityǁ         0.00017809          45.153          3.3635          3.9606
v  Pressure                  -1972          220.39          21.427          38.808
v  k                   9.8289e-017        0.016825      0.00045573      0.00079369
v  omega                  0.000893       2.74e+008     1.3266e+006           78860
v  TempK                    298.15          362.73          298.47          299.07
v  TurbVisc            1.8872e-024      0.00031066     1.1906e-006     4.5228e-006
v  CourantNb           1.9468e-006               1         0.34019         0.34842
v  FourierNb              0.001732               1        0.073012        0.014331
v  total_pressure            99353     1.0155e+005     1.0135e+005     1.0136e+005
v  Local Time Step     1.2848e-006     7.4002e-005     3.8767e-005     6.9684e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          362.52          300.79          303.08
v  Yplus               0          3.7718         0.37774         0.26213


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0073468          1.8994          0.4132         0.36275


 INSTANT    0.220000000E-03   TIME STEP NUMBER              22
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925371E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17458E-01 0.65400E+01
   Friction velocity        uk    :  0.17458E-01 0.65391E+01
   Dimensionless distance   yplus :  0.10018E-01 0.38046E+01
   Friction thermal sca.    tstar : -0.45494E-08 0.11795E+02
   Rough dim-less th. sca.  tplus :  0.70969E-02 0.26952E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        130 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24245E+00      11   0.74844E-05   0.23125E+03 0.78385E+03 
c  Velocity[X]                                      0.86398E+02 
c  Velocity[Y]                                      0.28516E+02 
c  Velocity[Z]                                      0.11634E+03 
c  Pressure     0.16187E-03      30   0.21464E-02   0.35342E+00 0.38394E+04 
c  k            0.96842E-04      10   0.14549E-04   0.15848E-03 0.93223E+03 
c  omega        0.28702E+07       3   0.50501E-06   0.16766E+13 0.36663E+03 
c  TempK        0.16320E+05       5   0.10264E-05   0.27998E+04 0.20354E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.5475e-006                           805
a  omega                  -0.60281                            19
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -21.707          25.824      -0.0041741      -0.0017601
v  Velocity[Y]             -21.006          21.056       0.0068567       0.0040531
v  Velocity[Z]              -44.22          16.586         -1.0136        -0.51559
v  ǁVelocityǁ         0.00017362          44.326          3.4058          3.9703
v  Pressure                  -1930          205.08          13.088          30.171
v  k                   5.5154e-016        0.017117      0.00046403      0.00081836
v  omega                  0.001061       2.74e+008     1.3206e+006           78308
v  TempK                    298.15          362.89           298.5          299.17
v  TurbVisc            2.4523e-024      0.00030255     1.1639e-006     4.4706e-006
v  CourantNb           2.0362e-006               1         0.36402         0.37782
v  FourierNb              0.001905               1         0.07995         0.01563
v  total_pressure            99395     1.0153e+005     1.0134e+005     1.0136e+005
v  Local Time Step     1.2848e-006     8.1403e-005     4.2047e-005     7.6301e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          362.73          300.92          303.33
v  Yplus               0          3.8046         0.37302         0.25637


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0080632          1.9284         0.44397         0.39345


 INSTANT    0.230000000E-03   TIME STEP NUMBER              23
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924998E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17240E-01 0.65700E+01
   Friction velocity        uk    :  0.17240E-01 0.65690E+01
   Dimensionless distance   yplus :  0.98930E-02 0.38220E+01
   Friction thermal sca.    tstar : -0.25540E-08 0.12388E+02
   Rough dim-less th. sca.  tplus :  0.70083E-02 0.27075E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        110 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22609E+00      11   0.80930E-05   0.22710E+03 0.74925E+03 
c  Velocity[X]                                      0.85814E+02 
c  Velocity[Y]                                      0.28128E+02 
c  Velocity[Z]                                      0.11315E+03 
c  Pressure     0.17185E-03      30   0.21179E-02   0.37313E+00 0.37073E+04 
c  k            0.94345E-04      10   0.15907E-04   0.16580E-03 0.85786E+03 
c  omega        0.28618E+07       3   0.46763E-06   0.11167E+13 0.28562E+03 
c  TempK        0.14896E+05       5   0.14013E-05   0.28814E+04 0.19695E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -3.1602e-006                           750
a  omega                  -0.83834                            19
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -23.248          27.125      -0.0040654      -0.0018724
v  Velocity[Y]             -20.508          20.661       0.0069817       0.0044505
v  Velocity[Z]             -43.337          17.518         -1.0334        -0.51544
v  ǁVelocityǁ         0.00016961          43.456           3.452           3.981
v  Pressure                -1889.3          196.36          4.7021          21.499
v  k                   1.6209e-015        0.017499      0.00047351       0.0008456
v  omega                 0.0011207       2.74e+008     1.3154e+006           77837
v  TempK                    298.15             363          298.54          299.28
v  TurbVisc            1.9577e-024      0.00028852      1.138e-006     4.4213e-006
v  CourantNb           2.1224e-006               1          0.3882         0.40857
v  FourierNb             0.0020954               1        0.087466        0.017022
v  total_pressure            99436     1.0152e+005     1.0133e+005     1.0135e+005
v  Local Time Step     1.2848e-006     8.9543e-005     4.5477e-005     8.3439e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          362.89          301.04          303.57
v  Yplus               0           3.822         0.36943         0.25131


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0088494           1.983         0.47567         0.42559


 INSTANT    0.240000000E-03   TIME STEP NUMBER              24
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924991E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17039E-01 0.65805E+01
   Friction velocity        uk    :  0.17039E-01 0.65794E+01
   Dimensionless distance   yplus :  0.97781E-02 0.38281E+01
   Friction thermal sca.    tstar : -0.37702E-11 0.12980E+02
   Rough dim-less th. sca.  tplus :  0.69268E-02 0.27118E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        104 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21185E+00      11   0.86572E-05   0.22253E+03 0.71746E+03 
c  Velocity[X]                                      0.85100E+02 
c  Velocity[Y]                                      0.27812E+02 
c  Velocity[Z]                                      0.10962E+03 
c  Pressure     0.16598E-03      30   0.21153E-02   0.35820E+00 0.32504E+04 
c  k            0.91874E-04      10   0.17212E-04   0.17393E-03 0.79136E+03 
c  omega        0.28542E+07       2   0.14244E-05   0.73790E+12 0.22165E+03 
c  TempK        0.13612E+05       5   0.19183E-05   0.29681E+04 0.19063E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -3.7659e-006                           671
a  omega                  -0.73717                            18
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -24.271          28.079        -0.00396      -0.0019903
v  Velocity[Y]             -19.965          20.166       0.0071308       0.0048792
v  Velocity[Z]             -42.427          16.493          -1.054         -0.5153
v  ǁVelocityǁ         0.00016803          42.554          3.5018          3.9927
v  Pressure                  -1833          194.54         -3.0422          13.487
v  k                   1.0733e-014        0.017722      0.00048432      0.00087566
v  omega                 0.0016572       2.74e+008     1.3112e+006           77437
v  TempK                    298.15          363.08          298.58           299.4
v  TurbVisc              4.03e-023      0.00028494     1.1132e-006     4.3731e-006
v  CourantNb           2.2145e-006               1         0.41257         0.44051
v  FourierNb             0.0020987               1        0.095588        0.018507
v  total_pressure            99492     1.0152e+005     1.0132e+005     1.0134e+005
v  Local Time Step     1.2848e-006     9.8497e-005     4.9037e-005      9.111e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15             363          301.16           303.8
v  Yplus               0          3.8281          0.3671         0.24693


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0097106          1.9705         0.50815         0.45902


 INSTANT    0.250000000E-03   TIME STEP NUMBER              25
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924864E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16960E-01 0.65739E+01
   Friction velocity        uk    :  0.16960E-01 0.65728E+01
   Dimensionless distance   yplus :  0.97324E-02 0.38242E+01
   Friction thermal sca.    tstar : -0.13953E-10 0.13570E+02
   Rough dim-less th. sca.  tplus :  0.68945E-02 0.27091E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        101 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19959E+00      12   0.81234E-05   0.21764E+03 0.68833E+03 
c  Velocity[X]                                      0.84390E+02 
c  Velocity[Y]                                      0.27535E+02 
c  Velocity[Z]                                      0.10572E+03 
c  Pressure     0.15566E-03      31   0.21016E-02   0.33377E+00 0.27867E+04 
c  k            0.89430E-04      10   0.18564E-04   0.18309E-03 0.73218E+03 
c  omega        0.28473E+07       2   0.13381E-05   0.50809E+12 0.17590E+03 
c  TempK        0.12460E+05       5   0.26240E-05   0.30604E+04 0.18456E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -4.0046e-006                           602
a  omega                   -0.8368                            13
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -24.723          28.468      -0.0038457      -0.0021085
v  Velocity[Y]              -19.36          19.566        0.007306       0.0053313
v  Velocity[Z]             -41.498           14.57         -1.0754        -0.51517
v  ǁVelocityǁ          0.0001684          41.656          3.5549          4.0052
v  Pressure                -1762.2          194.14         -10.118          6.1547
v  k                   6.1014e-015        0.017805      0.00049666      0.00090889
v  omega                 0.0012263     2.7401e+008     1.3076e+006           77091
v  TempK                    298.15          363.12          298.62          299.54
v  TurbVisc            1.1672e-022      0.00028869      1.092e-006     4.3336e-006
v  CourantNb           2.3129e-006               1         0.43692         0.47348
v  FourierNb              0.002098               1         0.10435        0.020089
v  total_pressure            99563     1.0152e+005     1.0131e+005     1.0133e+005
v  Local Time Step     1.2848e-006      0.00010835     5.2698e-005     9.9321e-005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.08          301.28          304.01
v  Yplus               0          3.8242           0.366         0.24322


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010653          1.9988         0.54127         0.49357


 INSTANT    0.260000000E-03   TIME STEP NUMBER              26
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924666E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16977E-01 0.65567E+01
   Friction velocity        uk    :  0.16977E-01 0.65555E+01
   Dimensionless distance   yplus :  0.97424E-02 0.38236E+01
   Friction thermal sca.    tstar : -0.37006E-10 0.14158E+02
   Rough dim-less th. sca.  tplus :  0.69016E-02 0.27086E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         98 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18918E+00      12   0.85425E-05   0.21219E+03 0.66104E+03 
c  Velocity[X]                                      0.83407E+02 
c  Velocity[Y]                                      0.27294E+02 
c  Velocity[Z]                                      0.10149E+03 
c  Pressure     0.14418E-03      30   0.20881E-02   0.30710E+00 0.23277E+04 
c  k            0.87011E-04      10   0.20400E-04   0.19329E-03 0.67939E+03 
c  omega        0.28410E+07       2   0.12788E-05   0.35550E+12 0.14102E+03 
c  TempK        0.11429E+05       6   0.15309E-05   0.31623E+04 0.17883E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.494e-006                           527
a  omega                  -0.92569                             8
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -25.123          28.455      -0.0037312      -0.0022244
v  Velocity[Y]             -18.717          18.874       0.0075146       0.0058094
v  Velocity[Z]             -40.714          14.221         -1.0972        -0.51506
v  ǁVelocityǁ         0.00016983          40.909          3.6109          4.0186
v  Pressure                -1681.6          195.26         -16.486        -0.45233
v  k                   1.8849e-015        0.017779      0.00051072      0.00094564
v  omega                0.00072991     2.7401e+008     1.3046e+006           76792
v  TempK                    298.15          363.16          298.66          299.69
v  TurbVisc            1.5272e-022      0.00031941     1.0723e-006     4.2977e-006
v  CourantNb           2.4287e-006               1         0.46096         0.50724
v  FourierNb              0.002101               1         0.11377        0.021765
v  total_pressure            99643     1.0152e+005     1.0131e+005     1.0132e+005
v  Local Time Step     1.2848e-006      0.00011918     5.6422e-005      0.00010807

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.12           301.4          304.21
v  Yplus               0          3.8236         0.36593          0.2401


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011686          1.9996         0.57473           0.529


 INSTANT    0.270000000E-03   TIME STEP NUMBER              27
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924259E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17046E-01 0.65373E+01
   Friction velocity        uk    :  0.17046E-01 0.65361E+01
   Dimensionless distance   yplus :  0.97818E-02 0.38414E+01
   Friction thermal sca.    tstar : -0.20373E-10 0.14746E+02
   Rough dim-less th. sca.  tplus :  0.69295E-02 0.27212E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        103 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18055E+00      12   0.89297E-05   0.20637E+03 0.63537E+03 
c  Velocity[X]                                      0.82293E+02 
c  Velocity[Y]                                      0.27058E+02 
c  Velocity[Z]                                      0.97015E+02 
c  Pressure     0.11651E-03      30   0.20790E-02   0.24637E+00 0.16851E+04 
c  k            0.84620E-04      11   0.22228E-04   0.20449E-03 0.63212E+03 
c  omega        0.28353E+07       2   0.12453E-05   0.25363E+12 0.11465E+03 
c  TempK        0.10515E+05       6   0.20622E-05   0.32671E+04 0.17323E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -4.6823e-006                           450
a  omega                  -0.95457                             6
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -25.319          28.579      -0.0036153      -0.0023447
v  Velocity[Y]             -18.531          18.825       0.0077523       0.0063116
v  Velocity[Z]             -40.265          14.134         -1.1193        -0.51498
v  ǁVelocityǁ          0.0001712          40.348          3.6694          4.0328
v  Pressure                -1594.4          195.22         -21.306         -5.4942
v  k                   5.3411e-016        0.017678      0.00052663      0.00098628
v  omega                  0.016971     2.7401e+008      1.302e+006           76534
v  TempK                    298.15          363.18          298.71          299.85
v  TurbVisc            4.7471e-023      0.00038946     1.0545e-006     4.2652e-006
v  CourantNb           2.6072e-006               1         0.48431         0.54141
v  FourierNb             0.0021076               1         0.12389        0.023532
v  total_pressure            99731     1.0152e+005      1.013e+005     1.0132e+005
v  Local Time Step     1.2848e-006       0.0001311     6.0166e-005      0.00011733

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.16          301.51           304.4
v  Yplus               0          3.8414         0.36676         0.23751


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012817          1.9828          0.6082         0.56495


 INSTANT    0.280000000E-03   TIME STEP NUMBER              28
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924342E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17109E-01 0.65098E+01
   Friction velocity        uk    :  0.17109E-01 0.65086E+01
   Dimensionless distance   yplus :  0.98179E-02 0.38463E+01
   Friction thermal sca.    tstar : -0.98048E-10 0.15331E+02
   Rough dim-less th. sca.  tplus :  0.69550E-02 0.27247E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        105 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17363E+00      12   0.92636E-05   0.20027E+03 0.61148E+03 
c  Velocity[X]                                      0.81021E+02 
c  Velocity[Y]                                      0.26822E+02 
c  Velocity[Z]                                      0.92426E+02 
c  Pressure     0.85313E-04      27   0.20397E-02   0.17897E+00 0.11454E+04 
c  k            0.82259E-04      11   0.24571E-04   0.21659E-03 0.58950E+03 
c  omega        0.28301E+07       2   0.12142E-05   0.18363E+12 0.94444E+02 
c  TempK        0.97115E+04       6   0.27977E-05   0.33775E+04 0.16783E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -4.6988e-006                           380
a  omega                   -1.0649                             6
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -25.352           28.41      -0.0035218      -0.0024761
v  Velocity[Y]             -18.389           18.89       0.0080055       0.0068288
v  Velocity[Z]             -39.917          13.962         -1.1415        -0.51492
v  ǁVelocityǁ         0.00017445          40.008            3.73          4.0477
v  Pressure                -1501.6          194.94         -24.398         -8.7876
v  k                   1.7208e-015        0.017535      0.00054448       0.0010312
v  omega                  0.085979     2.7402e+008     1.2998e+006           76309
v  TempK                    298.15          363.19          298.77          300.03
v  TurbVisc            1.3421e-023      0.00051031     1.0394e-006     4.2374e-006
v  CourantNb            2.849e-006               1         0.50656         0.57552
v  FourierNb             0.0021185               1         0.13474        0.025389
v  total_pressure            99823     1.0152e+005      1.013e+005     1.0132e+005
v  Local Time Step     1.2848e-006      0.00014421     6.3883e-005      0.00012705

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.18          301.61          304.56
v  Yplus               0          3.8463         0.36849         0.23544


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014057          1.9977          0.6413         0.60091


 INSTANT    0.290000000E-03   TIME STEP NUMBER              29
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924428E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17264E-01 0.64715E+01
   Friction velocity        uk    :  0.17264E-01 0.64702E+01
   Dimensionless distance   yplus :  0.99066E-02 0.38394E+01
   Friction thermal sca.    tstar : -0.49740E-09 0.15911E+02
   Rough dim-less th. sca.  tplus :  0.70179E-02 0.27198E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        117 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16839E+00      12   0.94389E-05   0.19376E+03 0.58881E+03 
c  Velocity[X]                                      0.79561E+02 
c  Velocity[Y]                                      0.26555E+02 
c  Velocity[Z]                                      0.87642E+02 
c  Pressure     0.61291E-04      28   0.20137E-02   0.12754E+00 0.80669E+03 
c  k            0.79932E-04      11   0.27070E-04   0.22948E-03 0.55075E+03 
c  omega        0.28253E+07       2   0.11729E-05   0.13422E+12 0.78680E+02 
c  TempK        0.90169E+04       6   0.37987E-05   0.34932E+04 0.16262E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -4.3065e-006                           323
a  omega                   -1.0409                             6
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -25.405          28.072      -0.0034347      -0.0026245
v  Velocity[Y]             -18.354          18.924       0.0082669       0.0073547
v  Velocity[Z]             -39.502          13.775         -1.1636        -0.51487
v  ǁVelocityǁ         0.00017845          39.599           3.792          4.0632
v  Pressure                -1406.6          194.49         -25.788         -10.357
v  k                   2.6922e-015        0.017608      0.00056429       0.0010809
v  omega                 0.0095065     2.7402e+008     1.2979e+006           76114
v  TempK                    298.15           363.2          298.82          300.23
v  TurbVisc            4.3302e-023      0.00046192     1.0271e-006     4.2141e-006
v  CourantNb           3.1372e-006               1         0.52726          0.6089
v  FourierNb             0.0021337               1         0.14638        0.027333
v  total_pressure            99918     1.0152e+005      1.013e+005     1.0131e+005
v  Local Time Step     1.1678e-006      0.00015863     6.7541e-005      0.00013716

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.19          301.72          304.71
v  Yplus               0          3.8394         0.37109         0.23386


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015417          1.9981         0.67364         0.63624


 INSTANT    0.300000000E-03   TIME STEP NUMBER              30
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924039E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17454E-01 0.64226E+01
   Friction velocity        uk    :  0.17454E-01 0.64214E+01
   Dimensionless distance   yplus :  0.10016E-01 0.38244E+01
   Friction thermal sca.    tstar : -0.23296E-08 0.16486E+02
   Rough dim-less th. sca.  tplus :  0.70954E-02 0.27092E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        125 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16462E+00      12   0.95609E-05   0.18714E+03 0.56740E+03 
c  Velocity[X]                                      0.77989E+02 
c  Velocity[Y]                                      0.26274E+02 
c  Velocity[Z]                                      0.82875E+02 
c  Pressure     0.57094E-04      26   0.19781E-02   0.11788E+00 0.72888E+03 
c  k            0.77638E-04      11   0.30652E-04   0.24311E-03 0.51533E+03 
c  omega        0.28210E+07       2   0.11144E-05   0.98355E+11 0.65988E+02 
c  TempK        0.84257E+04       7   0.25863E-05   0.36179E+04 0.15770E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -3.8541e-006                           252
a  omega                   -1.0331                             4
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -25.354          27.706      -0.0033567      -0.0027761
v  Velocity[Y]             -18.205           19.27       0.0085392       0.0078969
v  Velocity[Z]             -39.016          13.499         -1.1854        -0.51477
v  ǁVelocityǁ         0.00018255          39.119          3.8549          4.0792
v  Pressure                -1313.4           194.6         -25.369         -10.099
v  k                   8.3572e-017        0.017584        0.000586       0.0011357
v  omega                  0.015359     2.7402e+008     1.2963e+006           75944
v  TempK                    298.15           363.2          298.89          300.44
v  TurbVisc            6.7674e-023      0.00052473     1.0175e-006     4.1931e-006
v  CourantNb           3.4417e-006               1         0.54642         0.64112
v  FourierNb             0.0021533               1         0.15887         0.02937
v  total_pressure      1.0001e+005     1.0152e+005      1.013e+005     1.0131e+005
v  Local Time Step      1.066e-006      0.00017449     7.1142e-005      0.00014757

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15           363.2          301.82          304.84
v  Yplus               0          3.8244         0.37442         0.23272


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016902          1.9994         0.70529         0.67049


 INSTANT    0.310000000E-03   TIME STEP NUMBER              31
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924040E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17646E-01 0.63643E+01
   Friction velocity        uk    :  0.17646E-01 0.63630E+01
   Dimensionless distance   yplus :  0.10126E-01 0.38030E+01
   Friction thermal sca.    tstar : -0.12454E-07 0.17055E+02
   Rough dim-less th. sca.  tplus :  0.71733E-02 0.26941E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        134 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16204E+00      12   0.96342E-05   0.18047E+03 0.54704E+03 
c  Velocity[X]                                      0.76346E+02 
c  Velocity[Y]                                      0.25940E+02 
c  Velocity[Z]                                      0.78185E+02 
c  Pressure     0.69114E-04      30   0.19131E-02   0.14166E+00 0.82957E+03 
c  k            0.75375E-04      11   0.37282E-04   0.25730E-03 0.48286E+03 
c  omega        0.28171E+07       2   0.10345E-05   0.71648E+11 0.55299E+02 
c  TempK        0.79295E+04       7   0.34006E-05   0.37424E+04 0.15288E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -4.0638e-006                           201
a  omega                  -0.85376                             2
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -25.211          27.322      -0.0032976      -0.0029201
v  Velocity[Y]             -18.194          19.647       0.0088204       0.0084574
v  Velocity[Z]             -38.461          13.366         -1.2067        -0.51463
v  ǁVelocityǁ         0.00018311          38.569          3.9183          4.0956
v  Pressure                -1226.7          194.88         -23.448          -8.312
v  k                   7.3625e-015        0.017465      0.00060954       0.0011964
v  omega                 0.0050179     2.7402e+008      1.295e+006           75795
v  TempK                    298.15           363.2          298.95          300.68
v  TurbVisc            2.0985e-024      0.00046658     1.0117e-006     4.1779e-006
v  CourantNb           3.7874e-006               1         0.56411         0.67194
v  FourierNb             0.0021766               1         0.17228        0.031506
v  total_pressure       1.001e+005     1.0152e+005      1.013e+005     1.0132e+005
v  Local Time Step     1.0035e-006      0.00019194     7.4687e-005      0.00015823

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15           363.2          301.91          304.96
v  Yplus               0           3.803         0.37827         0.23198


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018528          1.9997         0.73639         0.70345


 INSTANT    0.320000000E-03   TIME STEP NUMBER              32
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924732E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17433E-01 0.62929E+01
   Friction velocity        uk    :  0.17433E-01 0.62916E+01
   Dimensionless distance   yplus :  0.10133E-01 0.37755E+01
   Friction thermal sca.    tstar : -0.56702E-07 0.17607E+02
   Rough dim-less th. sca.  tplus :  0.71786E-02 0.26746E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        139 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16038E+00      12   0.97098E-05   0.17393E+03 0.52791E+03 
c  Velocity[X]                                      0.74728E+02 
c  Velocity[Y]                                      0.25481E+02 
c  Velocity[Z]                                      0.73724E+02 
c  Pressure     0.85843E-04      29   0.18554E-02   0.17475E+00 0.93867E+03 
c  k            0.73131E-04      12   0.45320E-04   0.27179E-03 0.45309E+03 
c  omega        0.28136E+07       2   0.95023E-06   0.52299E+11 0.46475E+02 
c  TempK        0.75188E+04       7   0.44637E-05   0.38680E+04 0.14824E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -4.0791e-006                           153
a  omega                  -0.59231                             1
a  TempK          
a  Local Time Step     9.6702e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -24.967          26.806      -0.0032656      -0.0030503
v  Velocity[Y]             -18.398              20       0.0091107       0.0090458
v  Velocity[Z]             -37.842          13.162         -1.2276        -0.51447
v  ǁVelocityǁ         0.00018502          37.952          3.9818          4.1123
v  Pressure                  -1150          194.42         -20.417         -5.3868
v  k                   8.7919e-015        0.025918      0.00063474       0.0012632
v  omega                   0.13204     2.7403e+008     1.2938e+006           75667
v  TempK                    298.15           363.2          299.03          300.94
v  TurbVisc            1.8463e-022      0.00044393     1.0122e-006     4.1806e-006
v  CourantNb           4.1518e-006          1.0341         0.58045         0.70124
v  FourierNb             0.0022062               1         0.18657        0.033758
v  total_pressure      1.0017e+005     1.0152e+005      1.013e+005     1.0132e+005
v  Local Time Step          1e-006      0.00021114     7.8185e-005       0.0001691

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15           363.2          302.01          305.05
v  Yplus               0          3.7755          0.3825          0.2316


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.020307          1.9997         0.76702           0.735


 INSTANT    0.330000000E-03   TIME STEP NUMBER              33
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924075E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17745E-01 0.62089E+01
   Friction velocity        uk    :  0.17745E-01 0.62077E+01
   Dimensionless distance   yplus :  0.10183E-01 0.37433E+01
   Friction thermal sca.    tstar : -0.22301E-06 0.18146E+02
   Rough dim-less th. sca.  tplus :  0.72137E-02 0.26518E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        136 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.15938E+00      12   0.96970E-05   0.16758E+03 0.50973E+03 
c  Velocity[X]                                      0.73043E+02 
c  Velocity[Y]                                      0.24918E+02 
c  Velocity[Z]                                      0.69618E+02 
c  Pressure     0.10504E-03      30   0.18077E-02   0.21252E+00 0.10568E+04 
c  k            0.70879E-04      12   0.53294E-04   0.28622E-03 0.42586E+03 
c  omega        0.28103E+07       2   0.88034E-06   0.38841E+11 0.39656E+02 
c  TempK        0.71833E+04       8   0.33612E-05   0.39963E+04 0.14388E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -3.9735e-006                           107
a  omega                 -0.083412                             1
a  TempK          
a  Local Time Step     9.4713e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -24.58          26.165      -0.0032336      -0.0031647
v  Velocity[Y]             -18.685          20.348       0.0094057       0.0096636
v  Velocity[Z]             -37.166          12.838          -1.248        -0.51429
v  ǁVelocityǁ         0.00018612          37.276          4.0453          4.1293
v  Pressure                  -1074          194.99         -16.292         -1.3495
v  k                   3.8739e-015         0.04165      0.00066145       0.0013366
v  omega                  0.083412     2.7403e+008     1.2928e+006           75554
v  TempK                    298.15          363.19          299.11          301.22
v  TurbVisc            1.9701e-022      0.00040273     1.0205e-006     4.2086e-006
v  CourantNb           4.5365e-006          1.0558         0.59563         0.72897
v  FourierNb             0.0022425               1         0.20188         0.03615
v  total_pressure      1.0025e+005     1.0152e+005     1.0131e+005     1.0132e+005
v  Local Time Step          1e-006      0.00023225     8.1652e-005      0.00018014

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15           363.2           302.1          305.13
v  Yplus               0          3.7433         0.38702         0.23156


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.022248               2         0.79752         0.76512


 INSTANT    0.340000000E-03   TIME STEP NUMBER              34
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924130E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17676E-01 0.61149E+01
   Friction velocity        uk    :  0.17676E-01 0.61137E+01
   Dimensionless distance   yplus :  0.10209E-01 0.37068E+01
   Friction thermal sca.    tstar : -0.84069E-06 0.18677E+02
   Rough dim-less th. sca.  tplus :  0.72320E-02 0.26259E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        135 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.15885E+00      12   0.96628E-05   0.16119E+03 0.49226E+03 
c  Velocity[X]                                      0.71193E+02 
c  Velocity[Y]                                      0.24241E+02 
c  Velocity[Z]                                      0.65759E+02 
c  Pressure     0.11729E-03      29   0.17437E-02   0.23586E+00 0.10793E+04 
c  k            0.68604E-04      12   0.62629E-04   0.30021E-03 0.40087E+03 
c  omega        0.28074E+07       2   0.82873E-06   0.29821E+11 0.34803E+02 
c  TempK        0.69131E+04       8   0.42741E-05   0.41164E+04 0.13966E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -3.6522e-006                            81
a  omega          
a  TempK          
a  Local Time Step      9.397e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -24.143          25.348      -0.0031871      -0.0032539
v  Velocity[Y]             -18.937          20.695       0.0097131        0.010313
v  Velocity[Z]             -36.446          12.447         -1.2681        -0.51409
v  ǁVelocityǁ         0.00018696          36.613          4.1086          4.1467
v  Pressure                -1004.5          201.55         -11.599          3.2709
v  k                    2.592e-015         0.06907       0.0006895       0.0014168
v  omega                   0.28782     2.7403e+008      1.292e+006           75457
v  TempK                    298.14          363.19          299.19          301.53
v  TurbVisc            9.5759e-023      0.00037577     1.0377e-006     4.2664e-006
v  CourantNb           4.9632e-006          1.0642         0.60979         0.75511
v  FourierNb             0.0022852               1         0.21816        0.038696
v  total_pressure      1.0032e+005     1.0153e+005     1.0131e+005     1.0133e+005
v  Local Time Step          1e-006      0.00025548     8.5084e-005      0.00019129

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.19          302.19           305.2
v  Yplus               0          3.7068         0.39178         0.23181


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.024365          1.9999         0.82795         0.79381


 INSTANT    0.350000000E-03   TIME STEP NUMBER              35
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924250E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11615E-01 0.60142E+01
   Friction velocity        uk    :  0.11615E-01 0.60131E+01
   Dimensionless distance   yplus :  0.83188E-02 0.36687E+01
   Friction thermal sca.    tstar : -0.29067E-05 0.19187E+02
   Rough dim-less th. sca.  tplus :  0.58931E-02 0.25989E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        137 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.15866E+00      12   0.96125E-05   0.15493E+03 0.47544E+03 
c  Velocity[X]                                      0.69288E+02 
c  Velocity[Y]                                      0.23448E+02 
c  Velocity[Z]                                      0.62196E+02 
c  Pressure     0.12156E-03      31   0.16933E-02   0.24299E+00 0.10346E+04 
c  k            0.66333E-04      13   0.73045E-04   0.31359E-03 0.37782E+03 
c  omega        0.28047E+07       2   0.78127E-06   0.23252E+11 0.30968E+02 
c  TempK        0.66987E+04       8   0.53686E-05   0.42276E+04 0.13568E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.956e-006                            64
a  omega          
a  TempK          
a  Local Time Step     9.4141e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -23.768          24.569      -0.0031457      -0.0033198
v  Velocity[Y]             -19.142          20.962        0.010025        0.010984
v  Velocity[Z]             -35.698          12.528         -1.2877        -0.51387
v  ǁVelocityǁ         0.00012485          36.151          4.1716          4.1642
v  Pressure                -949.12          213.13         -6.7626          8.0537
v  k                   8.9756e-015         0.10693      0.00071876       0.0015042
v  omega                   0.30465     2.7403e+008     1.2913e+006           75373
v  TempK                    298.14          363.29          299.29          301.87
v  TurbVisc            6.4847e-023      0.00046074     1.0643e-006     4.3583e-006
v  CourantNb           5.4356e-006          1.0622         0.62301         0.77959
v  FourierNb             0.0023315               1         0.23545        0.041413
v  total_pressure      1.0038e+005     1.0154e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006      0.00028102     8.8471e-005      0.00020249

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.19          302.27          305.25
v  Yplus               0          3.6687         0.39666         0.23235


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.026668          1.9999         0.85846           0.821


 INSTANT    0.360000000E-03   TIME STEP NUMBER              36
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924513E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12743E-01 0.59175E+01
   Friction velocity        uk    :  0.12743E-01 0.59165E+01
   Dimensionless distance   yplus :  0.91440E-02 0.36303E+01
   Friction thermal sca.    tstar : -0.94713E-05 0.19667E+02
   Rough dim-less th. sca.  tplus :  0.64777E-02 0.25717E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        141 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.15871E+00      12   0.95091E-05   0.14870E+03 0.45917E+03 
c  Velocity[X]                                      0.67253E+02 
c  Velocity[Y]                                      0.22527E+02 
c  Velocity[Z]                                      0.58920E+02 
c  Pressure     0.12215E-03      30   0.16406E-02   0.24268E+00 0.96025E+03 
c  k            0.64104E-04      13   0.81715E-04   0.32616E-03 0.35689E+03 
c  omega        0.28023E+07       2   0.73197E-06   0.18254E+11 0.27717E+02 
c  TempK        0.65325E+04       9   0.43263E-05   0.43278E+04 0.13207E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.8343e-006                            45
a  omega          
a  TempK          
a  Local Time Step     9.4889e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -23.375          23.811      -0.0031085      -0.0033553
v  Velocity[Y]             -19.291          21.155        0.010348        0.011667
v  Velocity[Z]             -35.183          13.103          -1.307        -0.51366
v  ǁVelocityǁ        7.3086e-005          35.649          4.2342           4.182
v  Pressure                -908.41           224.3         -1.9764          12.809
v  k                   4.0373e-014         0.14825      0.00074904       0.0015986
v  omega                   0.32285     2.7404e+008     1.2908e+006           75300
v  TempK                    298.13          363.35          299.38          302.23
v  TurbVisc            2.2187e-022      0.00043189     1.1011e-006       4.49e-006
v  CourantNb            5.959e-006          1.0539         0.63524         0.80221
v  FourierNb             0.0023794               1         0.25265        0.044233
v  total_pressure      1.0042e+005     1.0155e+005     1.0132e+005     1.0134e+005
v  Local Time Step          1e-006      0.00030913      9.176e-005      0.00021362

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.29          302.36           305.3
v  Yplus               0          3.6303         0.40165         0.23318


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.029176          1.9999         0.88789         0.84644


 INSTANT    0.370000000E-03   TIME STEP NUMBER              37
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924566E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10151E-01 0.58595E+01
   Friction velocity        uk    :  0.10151E-01 0.58585E+01
   Dimensionless distance   yplus :  0.72841E-02 0.35898E+01
   Friction thermal sca.    tstar : -0.29057E-04 0.20121E+02
   Rough dim-less th. sca.  tplus :  0.51601E-02 0.25431E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        146 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.15893E+00      12   0.93208E-05   0.14273E+03 0.44359E+03 
c  Velocity[X]                                      0.65317E+02 
c  Velocity[Y]                                      0.21514E+02 
c  Velocity[Z]                                      0.55896E+02 
c  Pressure     0.11492E-03      30   0.16049E-02   0.22687E+00 0.83562E+03 
c  k            0.61969E-04      14   0.82029E-04   0.33718E-03 0.33815E+03 
c  omega        0.28001E+07       2   0.69435E-06   0.14750E+11 0.25564E+02 
c  TempK        0.64063E+04       9   0.50658E-05   0.44023E+04 0.12873E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -7.6311e-007                            33
a  omega          
a  TempK          
a  Local Time Step     9.5952e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.963           23.02      -0.0030864      -0.0033535
v  Velocity[Y]             -19.377          21.372        0.010676        0.012356
v  Velocity[Z]             -34.724          13.288         -1.3261        -0.51346
v  ǁVelocityǁ         0.00013668          35.186          4.2964          4.1998
v  Pressure                -868.87          234.75          2.3598          17.134
v  k                   2.2799e-015         0.17652      0.00078016       0.0016999
v  omega                    0.3438     2.7404e+008     1.2903e+006           75238
v  TempK                    298.12          363.38          299.48          302.61
v  TurbVisc            1.0046e-021       0.0003452     1.1477e-006     4.6668e-006
v  CourantNb           6.5441e-006          1.0422         0.64649         0.82294
v  FourierNb             0.0024254               1         0.26886        0.047086
v  total_pressure      1.0046e+005     1.0156e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006      0.00034004     9.4913e-005      0.00022459

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.35          302.44          305.33
v  Yplus               0          3.5898         0.40668         0.23427


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.03191               2         0.91535         0.87002


 INSTANT    0.380000000E-03   TIME STEP NUMBER              38
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924529E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12791E-01 0.57918E+01
   Friction velocity        uk    :  0.12791E-01 0.57909E+01
   Dimensionless distance   yplus :  0.91782E-02 0.35430E+01
   Friction thermal sca.    tstar : -0.77733E-04 0.20546E+02
   Rough dim-less th. sca.  tplus :  0.65019E-02 0.25099E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        157 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.15926E+00      12   0.90851E-05   0.13694E+03 0.42878E+03 
c  Velocity[X]                                      0.63414E+02 
c  Velocity[Y]                                      0.20422E+02 
c  Velocity[Z]                                      0.53106E+02 
c  Pressure     0.98037E-04      32   0.15417E-02   0.19235E+00 0.66555E+03 
c  k            0.59999E-04      14   0.82551E-04   0.34675E-03 0.32171E+03 
c  omega        0.27982E+07       2   0.66879E-06   0.12236E+11 0.24272E+02 
c  TempK        0.63123E+04       9   0.57271E-05   0.44482E+04 0.12578E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -4.0749e-010                            17
a  omega          
a  TempK          
a  Local Time Step     9.7152e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.528           22.58      -0.0030972      -0.0033215
v  Velocity[Y]             -19.396          21.534        0.011027        0.013039
v  Velocity[Z]             -34.263          13.057         -1.3448        -0.51328
v  ǁVelocityǁ           0.000193          34.723          4.3581          4.2178
v  Pressure                 -836.1          243.75          5.8059          20.579
v  k                   2.2016e-014         0.18272       0.0008119       0.0018074
v  omega                   0.36776     2.7404e+008     1.2899e+006           75184
v  TempK                    298.11           363.4          299.58          303.02
v  TurbVisc             5.715e-023      0.00032216     1.2035e-006     4.8919e-006
v  CourantNb           7.2224e-006          1.0293         0.65689         0.84182
v  FourierNb             0.0024487               1         0.28483        0.050041
v  total_pressure      1.0049e+005     1.0157e+005     1.0133e+005     1.0135e+005
v  Local Time Step          1e-006      0.00037404     9.7947e-005      0.00023535

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.38          302.52          305.36
v  Yplus               0           3.543         0.41172         0.23562


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.034889               2         0.94172         0.89186


 INSTANT    0.390000000E-03   TIME STEP NUMBER              39
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924645E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96611E-02 0.57192E+01
   Friction velocity        uk    :  0.96611E-02 0.57183E+01
   Dimensionless distance   yplus :  0.65504E-02 0.34974E+01
   Friction thermal sca.    tstar : -0.18909E-03 0.20940E+02
   Rough dim-less th. sca.  tplus :  0.46403E-02 0.24776E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        168 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.15966E+00      12   0.88358E-05   0.13133E+03 0.41466E+03 
c  Velocity[X]                                      0.61504E+02 
c  Velocity[Y]                                      0.19290E+02 
c  Velocity[Z]                                      0.50539E+02 
c  Pressure     0.72114E-04      28   0.14994E-02   0.14069E+00 0.45444E+03 
c  k            0.58282E-04      14   0.86450E-04   0.35463E-03 0.30689E+03 
c  omega        0.27964E+07       2   0.64370E-06   0.10302E+11 0.22979E+02 
c  TempK        0.62443E+04      10   0.44972E-05   0.44639E+04 0.12330E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.9912e-010                            11
a  omega          
a  TempK          
a  Local Time Step      9.834e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.032          22.082      -0.0031491      -0.0032636
v  Velocity[Y]             -19.339           21.63        0.011395         0.01372
v  Velocity[Z]             -33.772          12.753         -1.3631        -0.51312
v  ǁVelocityǁ         0.00019824          34.229          4.4192          4.2358
v  Pressure                -806.94          250.85          7.7902          22.573
v  k                   1.7974e-014         0.16832      0.00084406       0.0019201
v  omega                   0.39491     2.7404e+008     1.2896e+006           75139
v  TempK                    298.09          363.41          299.69          303.44
v  TurbVisc            4.9314e-022      0.00029876     1.2678e-006     5.1626e-006
v  CourantNb           7.9681e-006          1.0169         0.66648         0.85895
v  FourierNb             0.0024755               1         0.29979        0.053007
v  total_pressure      1.0052e+005     1.0158e+005     1.0133e+005     1.0135e+005
v  Local Time Step          1e-006      0.00041145      0.00010083      0.00024583

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15           363.4           302.6          305.38
v  Yplus               0          3.4974         0.41676         0.23719


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.038128               2         0.96627         0.91196


 INSTANT    0.400000000E-03   TIME STEP NUMBER              40
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924561E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13656E-01 0.56435E+01
   Friction velocity        uk    :  0.13656E-01 0.56426E+01
   Dimensionless distance   yplus :  0.92592E-02 0.34701E+01
   Friction thermal sca.    tstar : -0.43273E-03 0.21309E+02
   Rough dim-less th. sca.  tplus :  0.65593E-02 0.24582E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        168 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16011E+00      12   0.85665E-05   0.12588E+03 0.40132E+03 
c  Velocity[X]                                      0.59607E+02 
c  Velocity[Y]                                      0.18151E+02 
c  Velocity[Z]                                      0.48119E+02 
c  Pressure     0.51324E-04      27   0.14814E-02   0.99670E-01 0.29961E+03 
c  k            0.56928E-04      14   0.86268E-04   0.36035E-03 0.29335E+03 
c  omega        0.27948E+07       2   0.56726E-06   0.72130E+10 0.18781E+02 
c  TempK        0.61963E+04      10   0.45997E-05   0.44406E+04 0.12120E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -3.2324e-011                             4
a  omega          
a  TempK          
a  Local Time Step     9.9449e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -21.517          21.691      -0.0032181      -0.0031946
v  Velocity[Y]             -19.468          21.661        0.011775        0.014387
v  Velocity[Z]             -33.263          12.324         -1.3809        -0.51297
v  ǁVelocityǁ         0.00020497          33.715          4.4798          4.2537
v  Pressure                 -781.9          256.72          8.1252          22.927
v  k                   1.7866e-014         0.14775      0.00087649       0.0020368
v  omega                   0.42553     2.7403e+008     1.2894e+006           75102
v  TempK                    298.07          363.38          299.79          303.88
v  TurbVisc            4.4839e-022      0.00027435     1.3359e-006     5.4674e-006
v  CourantNb           8.1508e-006          1.0055         0.67533         0.87441
v  FourierNb              0.002506               1          0.3144        0.056019
v  total_pressure      1.0054e+005     1.0158e+005     1.0133e+005     1.0135e+005
v  Local Time Step          1e-006      0.00045259      0.00010357      0.00025597

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.41          302.68          305.39
v  Yplus               0          3.4701         0.42176         0.23895


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.041643               2         0.98972         0.93043


 INSTANT    0.410000000E-03   TIME STEP NUMBER              41
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924558E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17533E-01 0.55676E+01
   Friction velocity        uk    :  0.17533E-01 0.55667E+01
   Dimensionless distance   yplus :  0.10730E-01 0.34401E+01
   Friction thermal sca.    tstar : -0.91163E-03 0.21638E+02
   Rough dim-less th. sca.  tplus :  0.76013E-02 0.24370E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        160 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16058E+00      12   0.82771E-05   0.12059E+03 0.38885E+03 
c  Velocity[X]                                      0.57682E+02 
c  Velocity[Y]                                      0.17049E+02 
c  Velocity[Z]                                      0.45858E+02 
c  Pressure     0.54173E-04      37   0.14487E-02   0.10476E+00 0.32765E+03 
c  k            0.56072E-04      14   0.81072E-04   0.36334E-03 0.28099E+03 
c  omega        0.27935E+07       2   0.52510E-06   0.57819E+10 0.16896E+02 
c  TempK        0.61645E+04      10   0.46091E-05   0.43799E+04 0.11954E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.7338e-011                             4
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -21.036          21.357      -0.0032876      -0.0031128
v  Velocity[Y]             -19.843          21.977        0.012177        0.015046
v  Velocity[Z]             -32.743           11.86         -1.3982        -0.51279
v  ǁVelocityǁ          0.0001441          33.187          4.5393          4.2715
v  Pressure                -758.79          260.62          6.6823          21.507
v  k                   3.2648e-014         0.12877      0.00090904       0.0021559
v  omega                   0.46006     2.7402e+008     1.2892e+006           75070
v  TempK                    298.06          363.35           299.9          304.33
v  TurbVisc            4.4514e-022       0.0002997     1.4008e-006     5.7841e-006
v  CourantNb           7.3487e-006               1         0.68348         0.88825
v  FourierNb             0.0025397               1         0.32784        0.058946
v  total_pressure      1.0057e+005     1.0159e+005     1.0133e+005     1.0135e+005
v  Local Time Step     1.0041e-006      0.00049785      0.00010615      0.00026568

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.38          302.75           305.4
v  Yplus               0          3.4401         0.42672         0.24089


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.045448               2          1.0113         0.94719


 INSTANT    0.420000000E-03   TIME STEP NUMBER              42
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924399E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14172E-01 0.54942E+01
   Friction velocity        uk    :  0.14172E-01 0.54933E+01
   Dimensionless distance   yplus :  0.10169E-01 0.34097E+01
   Friction thermal sca.    tstar : -0.17912E-02 0.21935E+02
   Rough dim-less th. sca.  tplus :  0.72037E-02 0.24155E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        179 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16107E+00      12   0.80339E-05   0.11551E+03 0.37711E+03 
c  Velocity[X]                                      0.55743E+02 
c  Velocity[Y]                                      0.16028E+02 
c  Velocity[Z]                                      0.43740E+02 
c  Pressure     0.73991E-04      31   0.14172E-02   0.14250E+00 0.47448E+03 
c  k            0.55847E-04      14   0.75413E-04   0.36420E-03 0.27016E+03 
c  omega        0.27929E+07       2   0.49416E-06   0.47473E+10 0.15531E+02 
c  TempK        0.61461E+04      10   0.45310E-05   0.42851E+04 0.11832E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -3.0081e-013                             4
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -21.918          21.028      -0.0033631      -0.0030354
v  Velocity[Y]             -20.096          22.405        0.012605        0.015702
v  Velocity[Z]              -32.22          11.526         -1.4149        -0.51258
v  ǁVelocityǁ         0.00019036          32.654           4.598          4.2892
v  Pressure                -740.14          261.58          3.8094           18.67
v  k                   1.7117e-013         0.12602      0.00094163       0.0022759
v  omega                   0.49909     2.7401e+008      1.289e+006           75045
v  TempK                    298.06          363.33             300          304.77
v  TurbVisc             8.161e-022      0.00024893     1.4584e-006     6.0901e-006
v  CourantNb           7.0287e-006               1         0.69101         0.90054
v  FourierNb             0.0025422               1         0.33917        0.061699
v  total_pressure      1.0058e+005     1.0159e+005     1.0133e+005     1.0134e+005
v  Local Time Step     1.0119e-006      0.00054764      0.00010854       0.0002749

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.35          302.82          305.41
v  Yplus               0          3.4097         0.43141         0.24295


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.049538               2          1.0302         0.96224


 INSTANT    0.430000000E-03   TIME STEP NUMBER              43
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924809E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16386E-01 0.54235E+01
   Friction velocity        uk    :  0.16386E-01 0.54227E+01
   Dimensionless distance   yplus :  0.10739E-01 0.33794E+01
   Friction thermal sca.    tstar : -0.33673E-02 0.22206E+02
   Rough dim-less th. sca.  tplus :  0.76073E-02 0.23940E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        190 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16156E+00      12   0.78163E-05   0.11062E+03 0.36621E+03 
c  Velocity[X]                                      0.53754E+02 
c  Velocity[Y]                                      0.15090E+02 
c  Velocity[Z]                                      0.41773E+02 
c  Pressure     0.90379E-04      31   0.14409E-02   0.17330E+00 0.59551E+03 
c  k            0.56389E-04      14   0.69897E-04   0.36405E-03 0.26135E+03 
c  omega        0.27929E+07       2   0.46701E-06   0.40214E+10 0.14320E+02 
c  TempK        0.61385E+04      10   0.43888E-05   0.41661E+04 0.11751E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -6.0357e-013                             3
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.673          21.228      -0.0034508      -0.0029318
v  Velocity[Y]             -20.309          22.782        0.013057        0.016375
v  Velocity[Z]               -31.7          11.453         -1.4311        -0.51233
v  ǁVelocityǁ         0.00017732           32.12          4.6556          4.3066
v  Pressure                -724.24          260.18       -0.026571           14.87
v  k                   4.9529e-014         0.11705      0.00097422       0.0023956
v  omega                   0.54336     2.7401e+008     1.2888e+006           75025
v  TempK                    298.05          363.32           300.1          305.21
v  TurbVisc            4.2898e-021      0.00022063     1.5059e-006     6.3653e-006
v  CourantNb           7.1163e-006               1           0.698         0.91127
v  FourierNb             0.0025433               1         0.34807        0.064148
v  total_pressure       1.006e+005     1.0159e+005     1.0132e+005     1.0134e+005
v  Local Time Step     1.0184e-006       0.0006024      0.00011071      0.00028349

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.33          302.89          305.42
v  Yplus               0          3.3794         0.43597         0.24512


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.053927               2          1.0461         0.97542


 INSTANT    0.440000000E-03   TIME STEP NUMBER              44
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924975E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15926E-01 0.53620E+01
   Friction velocity        uk    :  0.15926E-01 0.53612E+01
   Dimensionless distance   yplus :  0.10501E-01 0.33493E+01
   Friction thermal sca.    tstar : -0.59390E-02 0.22451E+02
   Rough dim-less th. sca.  tplus :  0.74390E-02 0.23727E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        176 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16205E+00      12   0.76113E-05   0.10597E+03 0.35616E+03 
c  Velocity[X]                                      0.51794E+02 
c  Velocity[Y]                                      0.14247E+02 
c  Velocity[Z]                                      0.39931E+02 
c  Pressure     0.10050E-03      31   0.14539E-02   0.19183E+00 0.66665E+03 
c  k            0.57744E-04      14   0.68592E-04   0.36404E-03 0.25489E+03 
c  omega        0.27929E+07       2   0.44315E-06   0.35061E+10 0.13401E+02 
c  TempK        0.61388E+04      10   0.41707E-05   0.40372E+04 0.11713E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -8.25e-013                             3
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -23.25          21.674      -0.0035467      -0.0027996
v  Velocity[Y]             -20.337          22.976        0.013518        0.017065
v  Velocity[Z]             -31.187          11.524         -1.4466        -0.51208
v  ǁVelocityǁ        5.8867e-005          31.592          4.7119          4.3239
v  Pressure                -711.25           256.8         -4.3825          10.553
v  k                   6.7797e-014         0.11477       0.0010068       0.0025144
v  omega                   0.59365     2.7401e+008     1.2887e+006           75009
v  TempK                    298.05           363.3           300.2          305.63
v  TurbVisc             1.227e-021      0.00022101      1.544e-006     6.5972e-006
v  CourantNb           7.2011e-006               1         0.70453         0.92033
v  FourierNb             0.0025438               1         0.35641         0.06642
v  total_pressure      1.0061e+005     1.0158e+005     1.0132e+005     1.0134e+005
v  Local Time Step     1.0234e-006      0.00066264      0.00011275      0.00029128

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.32          302.95          305.43
v  Yplus               0          3.3493         0.44027         0.24734


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.058629               2          1.0609         0.98675


 INSTANT    0.450000000E-03   TIME STEP NUMBER              45
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925047E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89907E-02 0.53172E+01
   Friction velocity        uk    :  0.89906E-02 0.53163E+01
   Dimensionless distance   yplus :  0.64512E-02 0.33201E+01
   Friction thermal sca.    tstar : -0.98457E-02 0.22672E+02
   Rough dim-less th. sca.  tplus :  0.45701E-02 0.23520E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        174 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16253E+00      12   0.74175E-05   0.10160E+03 0.34697E+03 
c  Velocity[X]                                      0.49877E+02 
c  Velocity[Y]                                      0.13488E+02 
c  Velocity[Z]                                      0.38235E+02 
c  Pressure     0.10141E-03      32   0.14852E-02   0.19265E+00 0.68018E+03 
c  k            0.59769E-04      14   0.66023E-04   0.36492E-03 0.25071E+03 
c  omega        0.27929E+07       2   0.42225E-06   0.31208E+10 0.12592E+02 
c  TempK        0.61452E+04      10   0.38991E-05   0.39098E+04 0.11725E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -9.2805e-013                             2
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -23.932           21.99      -0.0036497      -0.0026541
v  Velocity[Y]             -20.267          22.969        0.013983        0.017765
v  Velocity[Z]             -30.683          11.564         -1.4613        -0.51184
v  ǁVelocityǁ         3.449e-005          31.071          4.7668          4.3409
v  Pressure                -700.67          251.91         -8.8348          6.1429
v  k                   3.1935e-014         0.13746       0.0010395       0.0026318
v  omega                    0.6509       2.74e+008     1.2887e+006           74998
v  TempK                    298.02           363.3           300.3          306.04
v  TurbVisc            1.6991e-021      0.00024528     1.5736e-006      6.787e-006
v  CourantNb            7.369e-006               1         0.71051         0.92784
v  FourierNb              0.002544               1         0.36342        0.068397
v  total_pressure      1.0062e+005     1.0158e+005     1.0132e+005     1.0133e+005
v  Local Time Step     1.0275e-006       0.0007289      0.00011462      0.00029821

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15           363.3             303          305.43
v  Yplus               0          3.3201         0.44445         0.24968


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.048655               2          1.0739         0.99624


 INSTANT    0.460000000E-03   TIME STEP NUMBER              46
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925015E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69324E-02 0.52754E+01
   Friction velocity        uk    :  0.69324E-02 0.52746E+01
   Dimensionless distance   yplus :  0.49743E-02 0.32917E+01
   Friction thermal sca.    tstar : -0.15379E-01 0.22870E+02
   Rough dim-less th. sca.  tplus :  0.35238E-02 0.23318E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        178 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16301E+00      12   0.72036E-05   0.97455E+02 0.33851E+03 
c  Velocity[X]                                      0.48013E+02 
c  Velocity[Y]                                      0.12788E+02 
c  Velocity[Z]                                      0.36655E+02 
c  Pressure     0.98271E-04      33   0.15189E-02   0.18577E+00 0.66193E+03 
c  k            0.62262E-04      14   0.62924E-04   0.36734E-03 0.24881E+03 
c  omega        0.27929E+07       2   0.40700E-06   0.28528E+10 0.11984E+02 
c  TempK        0.61556E+04      10   0.36554E-05   0.37893E+04 0.11798E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -3.1517e-009                             3
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -24.508          22.196      -0.0037538      -0.0025018
v  Velocity[Y]               -20.1          22.756        0.014452         0.01848
v  Velocity[Z]             -30.191          11.549         -1.4754         -0.5116
v  ǁVelocityǁ        4.8059e-005          30.561          4.8202          4.3577
v  Pressure                -692.61          245.73         -13.164          1.8535
v  k                   1.2355e-013          0.1622       0.0010724       0.0027476
v  omega                   0.71617       2.74e+008     1.2886e+006           74992
v  TempK                    298.01           363.3          300.39          306.44
v  TurbVisc            8.0036e-022      0.00023595      1.596e-006     6.9423e-006
v  CourantNb           7.6018e-006               1         0.71601         0.93411
v  FourierNb             0.0025439               1         0.36978        0.070186
v  total_pressure      1.0063e+005     1.0157e+005     1.0131e+005     1.0133e+005
v  Local Time Step     1.0306e-006       0.0008018      0.00011638       0.0003044

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.29          303.05          305.44
v  Yplus               0          3.2917         0.44854         0.25213


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.070917               2          1.0858          1.0043


 INSTANT    0.470000000E-03   TIME STEP NUMBER              47
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925087E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81796E-02 0.52352E+01
   Friction velocity        uk    :  0.81796E-02 0.52343E+01
   Dimensionless distance   yplus :  0.58693E-02 0.32637E+01
   Friction thermal sca.    tstar : -0.22642E-01 0.23046E+02
   Rough dim-less th. sca.  tplus :  0.41578E-02 0.23120E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        187 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16348E+00      12   0.70005E-05   0.93559E+02 0.33092E+03 
c  Velocity[X]                                      0.46229E+02 
c  Velocity[Y]                                      0.12147E+02 
c  Velocity[Z]                                      0.35183E+02 
c  Pressure     0.96607E-04      30   0.15935E-02   0.18173E+00 0.65455E+03 
c  k            0.65037E-04      14   0.62987E-04   0.37230E-03 0.24937E+03 
c  omega        0.27928E+07       2   0.39362E-06   0.26538E+10 0.11520E+02 
c  TempK        0.61686E+04      10   0.34748E-05   0.36770E+04 0.11941E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -6.6924e-007                             8
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -25.008          22.322      -0.0038689      -0.0023488
v  Velocity[Y]             -19.812          22.495        0.014932        0.019213
v  Velocity[Z]             -29.712          11.488         -1.4887        -0.51137
v  ǁVelocityǁ        3.9615e-005          30.063          4.8718          4.3743
v  Pressure                 -687.6          238.71         -17.456         -2.4009
v  k                    1.551e-013            0.24       0.0011056       0.0028617
v  omega                    0.7908       2.74e+008     1.2886e+006           74989
v  TempK                    298.01           363.3          300.49          306.82
v  TurbVisc            3.0885e-021      0.00020545      1.612e-006      7.066e-006
v  CourantNb           7.7629e-006               1         0.72086         0.93942
v  FourierNb              0.002544               1         0.37476        0.071696
v  total_pressure      1.0064e+005     1.0156e+005     1.0131e+005     1.0132e+005
v  Local Time Step     1.0331e-006      0.00088197      0.00011799      0.00030998

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.28           303.1          305.44
v  Yplus               0          3.2637         0.45255          0.2547


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.078479               2          1.0956          1.0111


 INSTANT    0.480000000E-03   TIME STEP NUMBER              48
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925168E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.74333E-02 0.51957E+01
   Friction velocity        uk    :  0.74333E-02 0.51948E+01
   Dimensionless distance   yplus :  0.53337E-02 0.32363E+01
   Friction thermal sca.    tstar : -0.31487E-01 0.23202E+02
   Rough dim-less th. sca.  tplus :  0.37784E-02 0.22926E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        191 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16395E+00      12   0.68088E-05   0.89835E+02 0.32400E+03 
c  Velocity[X]                                      0.44517E+02 
c  Velocity[Y]                                      0.11551E+02 
c  Velocity[Z]                                      0.33767E+02 
c  Pressure     0.90672E-04      32   0.15607E-02   0.16969E+00 0.61688E+03 
c  k            0.67982E-04      14   0.72693E-04   0.38239E-03 0.25271E+03 
c  omega        0.27928E+07       2   0.37864E-06   0.24095E+10 0.11005E+02 
c  TempK        0.61830E+04      10   0.33256E-05   0.35725E+04 0.12157E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.226e-007                            22
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -25.406          22.361       -0.004009      -0.0022039
v  Velocity[Y]             -19.425           22.11        0.015406        0.019937
v  Velocity[Z]             -29.243          11.387         -1.5013        -0.51117
v  ǁVelocityǁ        4.2971e-005          29.576          4.9215          4.3905
v  Pressure                -690.66          231.96          -21.51          -6.422
v  k                   1.0243e-014         0.41387       0.0011393       0.0029739
v  omega                    0.8764     2.7399e+008     1.2886e+006           74989
v  TempK                    298.03          363.29          300.58          307.18
v  TurbVisc            3.4751e-021      0.00023367     1.6229e-006      7.163e-006
v  CourantNb           7.7006e-006               1         0.72512         0.94401
v  FourierNb             0.0025444               1         0.37899        0.073035
v  total_pressure      1.0063e+005     1.0156e+005      1.013e+005     1.0132e+005
v  Local Time Step     1.0353e-006      0.00097017      0.00011949       0.0003151

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.28          303.13          305.44
v  Yplus               0          3.2363         0.45643         0.25736


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.08568               2          1.1041           1.017


 INSTANT    0.490000000E-03   TIME STEP NUMBER              49
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925019E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76797E-02 0.51766E+01
   Friction velocity        uk    :  0.76797E-02 0.51756E+01
   Dimensionless distance   yplus :  0.55082E-02 0.32152E+01
   Friction thermal sca.    tstar : -0.41668E-01 0.23338E+02
   Rough dim-less th. sca.  tplus :  0.39020E-02 0.22777E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        162 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16440E+00      12   0.65994E-05   0.86346E+02 0.31757E+03 
c  Velocity[X]                                      0.42934E+02 
c  Velocity[Y]                                      0.11001E+02 
c  Velocity[Z]                                      0.32410E+02 
c  Pressure     0.81065E-04      30   0.15813E-02   0.15094E+00 0.54409E+03 
c  k            0.71047E-04      14   0.10254E-03   0.40158E-03 0.25917E+03 
c  omega        0.27928E+07       2   0.36194E-06   0.21096E+10 0.10260E+02 
c  TempK        0.61985E+04      10   0.31960E-05   0.34753E+04 0.12451E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -6.7551e-007                            45
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -25.695          22.431      -0.0041613      -0.0020645
v  Velocity[Y]             -19.004          21.708        0.015884        0.020643
v  Velocity[Z]             -28.843          11.255         -1.5132        -0.51098
v  ǁVelocityǁ        2.6461e-005           29.16          4.9693          4.4065
v  Pressure                -704.64          225.84          -25.07         -9.9535
v  k                   6.7152e-016         0.77094       0.0011737        0.003084
v  omega                   0.97491     2.7399e+008     1.2887e+006           74992
v  TempK                    298.03          363.29          300.68          307.53
v  TurbVisc            2.5573e-022      0.00024188     1.6296e-006     7.2394e-006
v  CourantNb           7.7127e-006               1          0.7287         0.94798
v  FourierNb             0.0025445               1         0.38189        0.074111
v  total_pressure      1.0062e+005     1.0155e+005      1.013e+005     1.0132e+005
v  Local Time Step     1.0371e-006       0.0010672      0.00012087      0.00031978

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.27          303.17          305.44
v  Yplus               0          3.2152          0.4602         0.26009


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.086587               2          1.1106          1.0221


 INSTANT    0.500000000E-03   TIME STEP NUMBER              50
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925194E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82037E-02 0.51893E+01
   Friction velocity        uk    :  0.82037E-02 0.51883E+01
   Dimensionless distance   yplus :  0.58840E-02 0.32133E+01
   Friction thermal sca.    tstar : -0.57312E-01 0.23458E+02
   Rough dim-less th. sca.  tplus :  0.41683E-02 0.22763E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        139 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16485E+00      12   0.63907E-05   0.83161E+02 0.31156E+03 
c  Velocity[X]                                      0.41522E+02 
c  Velocity[Y]                                      0.10487E+02 
c  Velocity[Z]                                      0.31152E+02 
c  Pressure     0.71091E-04      29   0.15758E-02   0.13171E+00 0.46935E+03 
c  k            0.74205E-04      14   0.16950E-03   0.44936E-03 0.27056E+03 
c  omega        0.27928E+07       2   0.34703E-06   0.18941E+10 0.96892E+01 
c  TempK        0.62146E+04      10   0.30633E-05   0.33844E+04 0.12824E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -8.9316e-007                            83
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -25.907           22.59       -0.004316      -0.0019409
v  Velocity[Y]             -18.627          21.419        0.016383        0.021347
v  Velocity[Z]             -28.639          11.106         -1.5243        -0.51081
v  ǁVelocityǁ        8.1386e-005           28.86          5.0151          4.4222
v  Pressure                -716.75          219.35         -28.118         -12.974
v  k                   1.0473e-014          1.3624       0.0012092       0.0031919
v  omega                    1.0294     2.7398e+008     1.2887e+006           74997
v  TempK                    298.04          363.29          300.78          307.86
v  TurbVisc            1.6752e-023      0.00021738     1.6334e-006     7.3014e-006
v  CourantNb            7.137e-006               1         0.73182         0.95145
v  FourierNb             0.0025445               1         0.38414        0.075038
v  total_pressure      1.0061e+005     1.0154e+005      1.013e+005     1.0131e+005
v  Local Time Step     1.0387e-006       0.0011739      0.00012217      0.00032409

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.27           303.2          305.45
v  Yplus               0          3.2133         0.46384          0.2629


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.099092               2           1.116          1.0265


 INSTANT    0.510000000E-03   TIME STEP NUMBER              51
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925168E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10269E-01 0.51976E+01
   Friction velocity        uk    :  0.10269E-01 0.51965E+01
   Dimensionless distance   yplus :  0.73655E-02 0.32184E+01
   Friction thermal sca.    tstar : -0.78155E-01 0.23562E+02
   Rough dim-less th. sca.  tplus :  0.52178E-02 0.22799E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        168 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16529E+00      12   0.62017E-05   0.80249E+02 0.30594E+03 
c  Velocity[X]                                      0.40240E+02 
c  Velocity[Y]                                      0.10007E+02 
c  Velocity[Z]                                      0.30002E+02 
c  Pressure     0.62125E-04      29   0.16183E-02   0.11452E+00 0.39844E+03 
c  k            0.77442E-04      14   0.23650E-03   0.50689E-03 0.28692E+03 
c  omega        0.27928E+07       2   0.33450E-06   0.17373E+10 0.92644E+01 
c  TempK        0.62312E+04       9   0.51631E-05   0.32943E+04 0.13258E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.0206e-006                           114
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -26.055            22.8      -0.0044553      -0.0018106
v  Velocity[Y]             -18.199          21.227        0.016886        0.022042
v  Velocity[Z]             -28.447          10.947         -1.5347        -0.51064
v  ǁVelocityǁ         0.00010484          28.662          5.0591          4.4375
v  Pressure                -726.73          212.89         -30.668         -15.496
v  k                   2.3405e-014          2.0583        0.001246       0.0032975
v  omega                    1.0886     2.7397e+008     1.2887e+006           75005
v  TempK                    298.05          363.28          300.87          308.17
v  TurbVisc            2.6452e-022      0.00018082     1.6354e-006     7.3549e-006
v  CourantNb           6.1377e-006               1         0.73444         0.95445
v  FourierNb             0.0025443               1         0.38531         0.07572
v  total_pressure       1.006e+005     1.0154e+005     1.0129e+005     1.0131e+005
v  Local Time Step       1.04e-006       0.0012913      0.00012335      0.00032801

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.26          303.22          305.45
v  Yplus               0          3.2184         0.46737         0.26577


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.10655               2          1.1197          1.0302


 INSTANT    0.520000000E-03   TIME STEP NUMBER              52
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925353E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11909E-01 0.51998E+01
   Friction velocity        uk    :  0.11909E-01 0.51985E+01
   Dimensionless distance   yplus :  0.80663E-02 0.32196E+01
   Friction thermal sca.    tstar : -0.10269E+00 0.23652E+02
   Rough dim-less th. sca.  tplus :  0.57142E-02 0.22808E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        178 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16573E+00      12   0.60204E-05   0.77652E+02 0.30075E+03 
c  Velocity[X]                                      0.39100E+02 
c  Velocity[Y]                                      0.95713E+01 
c  Velocity[Z]                                      0.28981E+02 
c  Pressure     0.53942E-04      28   0.15871E-02   0.98917E-01 0.33184E+03 
c  k            0.80743E-04      14   0.30890E-03   0.56895E-03 0.30747E+03 
c  omega        0.27928E+07       2   0.32333E-06   0.15891E+10 0.88616E+01 
c  TempK        0.62478E+04       9   0.49912E-05   0.32144E+04 0.13784E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.219e-006                           136
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -26.208          22.969      -0.0045884       -0.001671
v  Velocity[Y]             -17.829          20.945        0.017392        0.022723
v  Velocity[Z]             -28.263          10.785         -1.5445        -0.51048
v  ǁVelocityǁ        9.3085e-005          28.473          5.1013          4.4527
v  Pressure                   -734          205.52          -32.74         -17.541
v  k                   2.7311e-014          2.7632       0.0012845       0.0034008
v  omega                    1.1555     2.7397e+008     1.2888e+006           75014
v  TempK                    298.05          363.27          300.97          308.46
v  TurbVisc            5.9002e-022      0.00017647     1.6363e-006     7.4029e-006
v  CourantNb           4.9835e-006               1         0.73683         0.95708
v  FourierNb             0.0025439               1         0.38664         0.07641
v  total_pressure      1.0059e+005     1.0153e+005     1.0129e+005     1.0131e+005
v  Local Time Step     1.0409e-006       0.0014204      0.00012456      0.00033158

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.26          303.24          305.45
v  Yplus               0          3.2196         0.47079         0.26871


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.096049               2          1.1235          1.0335


 INSTANT    0.530000000E-03   TIME STEP NUMBER              53
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925044E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12226E-01 0.51954E+01
   Friction velocity        uk    :  0.12226E-01 0.51940E+01
   Dimensionless distance   yplus :  0.78608E-02 0.32169E+01
   Friction thermal sca.    tstar : -0.13037E+00 0.23730E+02
   Rough dim-less th. sca.  tplus :  0.55686E-02 0.22789E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        163 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16615E+00      11   0.73146E-05   0.75320E+02 0.29592E+03 
c  Velocity[X]                                      0.38072E+02 
c  Velocity[Y]                                      0.91715E+01 
c  Velocity[Z]                                      0.28076E+02 
c  Pressure     0.48335E-04      28   0.15189E-02   0.88173E-01 0.28110E+03 
c  k            0.84080E-04      14   0.28615E-03   0.56560E-03 0.32470E+03 
c  omega        0.27928E+07       2   0.31280E-06   0.14674E+10 0.84851E+01 
c  TempK        0.62643E+04       9   0.48381E-05   0.31385E+04 0.14385E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.3211e-006                           152
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -26.381          23.096      -0.0047139      -0.0015191
v  Velocity[Y]             -17.474          20.595        0.017895        0.023389
v  Velocity[Z]             -28.087          10.628         -1.5536        -0.51032
v  ǁVelocityǁ        6.4229e-005          28.292           5.142          4.4675
v  Pressure                -738.38           198.1         -34.438         -19.215
v  k                   3.4905e-015          3.2614       0.0013248       0.0035018
v  omega                    1.2297     2.7395e+008     1.2888e+006           75024
v  TempK                    298.07          363.26          301.07          308.73
v  TurbVisc            6.9076e-022      0.00017333     1.6369e-006     7.4492e-006
v  CourantNb           5.7415e-006               1         0.73903         0.95935
v  FourierNb             0.0025433               1         0.38816        0.077121
v  total_pressure      1.0059e+005     1.0152e+005     1.0129e+005     1.0131e+005
v  Local Time Step     1.0331e-006       0.0015625       0.0001258      0.00033477

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.25          303.25          305.45
v  Yplus               0          3.2169         0.47409         0.27168


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.1219               2          1.1272          1.0365


 INSTANT    0.540000000E-03   TIME STEP NUMBER              54
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925057E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11760E-01 0.51850E+01
   Friction velocity        uk    :  0.11760E-01 0.51836E+01
   Dimensionless distance   yplus :  0.75612E-02 0.32104E+01
   Friction thermal sca.    tstar : -0.16157E+00 0.23798E+02
   Rough dim-less th. sca.  tplus :  0.53564E-02 0.22743E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        159 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16657E+00      11   0.71525E-05   0.73317E+02 0.29157E+03 
c  Velocity[X]                                      0.37202E+02 
c  Velocity[Y]                                      0.88025E+01 
c  Velocity[Z]                                      0.27313E+02 
c  Pressure     0.44401E-04      25   0.14897E-02   0.80565E-01 0.24591E+03 
c  k            0.87390E-04      14   0.19010E-03   0.54518E-03 0.33992E+03 
c  omega        0.27928E+07       2   0.30223E-06   0.13183E+10 0.80224E+01 
c  TempK        0.62808E+04       9   0.46917E-05   0.30654E+04 0.15060E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.3614e-006                           157
a  omega          
a  TempK          
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -26.531          23.243      -0.0048375      -0.0013547
v  Velocity[Y]             -17.138          20.191        0.018405        0.024041
v  Velocity[Z]             -27.918          10.584         -1.5621        -0.51017
v  ǁVelocityǁ        2.2542e-005          28.119          5.1811          4.4821
v  Pressure                -740.27          190.77         -35.878         -20.634
v  k                   6.8927e-015          3.5232       0.0013673       0.0036005
v  omega                    1.2988     2.7394e+008     1.2889e+006           75035
v  TempK                    298.07          363.25          301.17          308.99
v  TurbVisc            8.8267e-023       0.0001714     1.6383e-006     7.4962e-006
v  CourantNb           7.0089e-006               1         0.74099          0.9613
v  FourierNb             0.0025426               1         0.38951        0.077786
v  total_pressure      1.0058e+005     1.0152e+005     1.0129e+005      1.013e+005
v  Local Time Step     1.0064e-006       0.0017187      0.00012697      0.00033759

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.24          303.27          305.45
v  Yplus               0          3.2104          0.4773         0.27468


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.12976               2          1.1305          1.0391


 INSTANT    0.550000000E-03   TIME STEP NUMBER              55
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925268E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11288E-01 0.51691E+01
   Friction velocity        uk    :  0.11288E-01 0.51675E+01
   Dimensionless distance   yplus :  0.72578E-02 0.32005E+01
   Friction thermal sca.    tstar : -0.19372E+00 0.23860E+02
   Rough dim-less th. sca.  tplus :  0.51415E-02 0.22672E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        142 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16697E+00      11   0.69936E-05   0.71502E+02 0.28753E+03 
c  Velocity[X]                                      0.36447E+02 
c  Velocity[Y]                                      0.84583E+01 
c  Velocity[Z]                                      0.26597E+02 
c  Pressure     0.41361E-04      26   0.15023E-02   0.74635E-01 0.21341E+03 
c  k            0.90678E-04      14   0.11045E-03   0.55589E-03 0.36115E+03 
c  omega        0.27928E+07       2   0.29246E-06   0.12085E+10 0.76867E+01 
c  TempK        0.62973E+04       9   0.45499E-05   0.29946E+04 0.15807E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.2381e-006                           167
a  omega          
a  TempK          
a  Local Time Step     9.8281e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -26.636          23.403      -0.0049519       -0.001178
v  Velocity[Y]             -16.838          19.909         0.01892        0.024689
v  Velocity[Z]             -27.758          10.592           -1.57        -0.51001
v  ǁVelocityǁ        7.0998e-005          27.956          5.2189          4.4964
v  Pressure                -739.77          183.64         -37.072         -21.812
v  k                   8.4796e-015          3.5838       0.0014122       0.0036971
v  omega                    1.3831     2.7392e+008      1.289e+006           75047
v  TempK                    298.08          363.24          301.27          309.23
v  TurbVisc            1.7367e-022      0.00017002     1.6413e-006     7.5454e-006
v  CourantNb           7.2147e-006          1.0175         0.74236         0.96286
v  FourierNb              0.002542               1          0.3893        0.078101
v  total_pressure      1.0059e+005     1.0151e+005     1.0129e+005      1.013e+005
v  Local Time Step          1e-006       0.0018906      0.00012776      0.00033988

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.24          303.28          305.45
v  Yplus               0          3.2005          0.4804          0.2777


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.13782               2          1.1317           1.041


 INSTANT    0.560000000E-03   TIME STEP NUMBER              56
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925308E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10750E-01 0.51479E+01
   Friction velocity        uk    :  0.10750E-01 0.51463E+01
   Dimensionless distance   yplus :  0.69114E-02 0.31873E+01
   Friction thermal sca.    tstar : -0.22512E+00 0.23914E+02
   Rough dim-less th. sca.  tplus :  0.48961E-02 0.22579E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        149 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16737E+00      11   0.68592E-05   0.69871E+02 0.28376E+03 
c  Velocity[X]                                      0.35793E+02 
c  Velocity[Y]                                      0.81428E+01 
c  Velocity[Z]                                      0.25935E+02 
c  Pressure     0.39783E-04      25   0.15569E-02   0.71375E-01 0.19464E+03 
c  k            0.93951E-04      14   0.10611E-03   0.59855E-03 0.38822E+03 
c  omega        0.27928E+07       2   0.28308E-06   0.10854E+10 0.73354E+01 
c  TempK        0.63135E+04       9   0.44227E-05   0.29262E+04 0.16626E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -9.3836e-007                           166
a  omega          
a  TempK          
a  Local Time Step     9.6214e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -26.688          23.593      -0.0050614     -0.00098607
v  Velocity[Y]             -16.498          19.575        0.019434        0.025335
v  Velocity[Z]             -27.606          11.003         -1.5773        -0.50985
v  ǁVelocityǁ        5.0031e-005          27.885          5.2554          4.5105
v  Pressure                -737.13          176.37          -38.12         -22.844
v  k                   5.1382e-015          3.4812       0.0014599       0.0037917
v  omega                    1.4843      2.739e+008      1.289e+006           75060
v  TempK                    298.09          363.24          301.38          309.45
v  TurbVisc            2.1365e-022       0.0001677     1.6464e-006     7.5983e-006
v  CourantNb           7.5376e-006          1.0393         0.74372         0.96419
v  FourierNb             0.0025413               1         0.38908        0.078408
v  total_pressure      1.0059e+005      1.015e+005     1.0129e+005      1.013e+005
v  Local Time Step          1e-006       0.0020797      0.00012842      0.00034176

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.23          303.29          305.45
v  Yplus               0          3.1873         0.48339         0.28072


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.14639               2          1.1328          1.0426


 INSTANT    0.570000000E-03   TIME STEP NUMBER              57
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925231E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83149E-02 0.51222E+01
   Friction velocity        uk    :  0.83149E-02 0.51205E+01
   Dimensionless distance   yplus :  0.59638E-02 0.31713E+01
   Friction thermal sca.    tstar : -0.25348E+00 0.23964E+02
   Rough dim-less th. sca.  tplus :  0.42248E-02 0.22466E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        146 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16777E+00      11   0.67598E-05   0.68404E+02 0.28024E+03 
c  Velocity[X]                                      0.35223E+02 
c  Velocity[Y]                                      0.78557E+01 
c  Velocity[Z]                                      0.25325E+02 
c  Pressure     0.37206E-04      24   0.14753E-02   0.66352E-01 0.16112E+03 
c  k            0.97216E-04      14   0.14571E-03   0.65680E-03 0.41876E+03 
c  omega        0.27928E+07       2   0.27412E-06   0.97934E+09 0.69947E+01 
c  TempK        0.63295E+04       9   0.43100E-05   0.28600E+04 0.17515E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -8.1688e-007                           168
a  omega          
a  TempK          
a  Local Time Step     9.4417e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -26.692          23.758      -0.0051577      -0.0007922
v  Velocity[Y]             -16.161          19.196        0.019952        0.025978
v  Velocity[Z]             -27.464          11.248         -1.5841        -0.50968
v  ǁVelocityǁ        3.1657e-005          27.867          5.2907          4.5244
v  Pressure                -732.24          169.07         -38.874         -23.586
v  k                   3.2918e-014           3.232       0.0015108       0.0038843
v  omega                    1.6011     2.7387e+008     1.2891e+006           75073
v  TempK                     298.1          363.23          301.49          309.65
v  TurbVisc            1.2982e-022      0.00016936     1.6535e-006      7.655e-006
v  CourantNb           7.6795e-006          1.0591         0.74504         0.96532
v  FourierNb             0.0025407               1          0.3888        0.078688
v  total_pressure      1.0059e+005     1.0149e+005     1.0129e+005      1.013e+005
v  Local Time Step          1e-006       0.0022876      0.00012888       0.0003432

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.22           303.3          305.45
v  Yplus               0          3.1713         0.48628         0.28375


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.15542               2          1.1338           1.044


 INSTANT    0.580000000E-03   TIME STEP NUMBER              58
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925118E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60911E-02 0.50921E+01
   Friction velocity        uk    :  0.60911E-02 0.50904E+01
   Dimensionless distance   yplus :  0.43688E-02 0.31527E+01
   Friction thermal sca.    tstar : -0.27699E+00 0.24005E+02
   Rough dim-less th. sca.  tplus :  0.30949E-02 0.22334E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        157 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16815E+00      11   0.66390E-05   0.67092E+02 0.27695E+03 
c  Velocity[X]                                      0.34701E+02 
c  Velocity[Y]                                      0.75951E+01 
c  Velocity[Z]                                      0.24796E+02 
c  Pressure     0.35400E-04      25   0.14659E-02   0.62736E-01 0.12701E+03 
c  k            0.10050E-03      14   0.18259E-03   0.72787E-03 0.45149E+03 
c  omega        0.27927E+07       2   0.26606E-06   0.91382E+09 0.67423E+01 
c  TempK        0.63452E+04       9   0.41970E-05   0.27963E+04 0.18472E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -7.9577e-007                           170
a  omega          
a  TempK          
a  Local Time Step     9.2865e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -26.66          23.895      -0.0052387     -0.00059188
v  Velocity[Y]              -15.95          18.785        0.020467        0.026626
v  Velocity[Z]             -27.331          11.554         -1.5904        -0.50952
v  ǁVelocityǁ        6.0372e-005          27.797          5.3248           4.538
v  Pressure                -725.65          162.14         -39.244         -23.943
v  k                    1.202e-014          2.8721       0.0015652       0.0039751
v  omega                    1.7342     2.7384e+008     1.2891e+006           75086
v  TempK                     298.1          363.22          301.61          309.84
v  TurbVisc            8.3477e-022      0.00017088     1.6627e-006     7.7155e-006
v  CourantNb           7.8951e-006          1.0768         0.74627         0.96627
v  FourierNb             0.0025401               1         0.38844        0.078931
v  total_pressure       1.006e+005     1.0149e+005     1.0129e+005      1.013e+005
v  Local Time Step          1e-006       0.0025164      0.00012909      0.00034416

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.22          303.31          305.45
v  Yplus               0          3.1527         0.48907         0.28676


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.16488               2          1.1347          1.0452


 INSTANT    0.590000000E-03   TIME STEP NUMBER              59
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925255E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87546E-02 0.50584E+01
   Friction velocity        uk    :  0.87546E-02 0.50567E+01
   Dimensionless distance   yplus :  0.56288E-02 0.31318E+01
   Friction thermal sca.    tstar : -0.29419E+00 0.34204E+02
   Rough dim-less th. sca.  tplus :  0.39875E-02 0.22186E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        145 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16852E+00      11   0.65182E-05   0.65931E+02 0.27395E+03 
c  Velocity[X]                                      0.34244E+02 
c  Velocity[Y]                                      0.73584E+01 
c  Velocity[Z]                                      0.24328E+02 
c  Pressure     0.35688E-04      24   0.14432E-02   0.62838E-01 0.11276E+03 
c  k            0.10382E-03      14   0.19252E-03   0.77738E-03 0.48375E+03 
c  omega        0.27927E+07       2   0.25887E-06   0.83873E+09 0.64972E+01 
c  TempK        0.63606E+04       9   0.40872E-05   0.27350E+04 0.19491E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -7.7216e-007                           164
a  omega          
a  TempK          
a  Local Time Step     9.1518e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -26.598          24.006      -0.0053022     -0.00038233
v  Velocity[Y]             -15.805          18.383        0.020985        0.027267
v  Velocity[Z]              -27.21          11.956         -1.5962        -0.50934
v  ǁVelocityǁ        5.5664e-005          27.682          5.3579          4.5514
v  Pressure                -717.83          155.73         -39.246         -23.936
v  k                   1.2844e-014          2.4601       0.0016233       0.0040642
v  omega                    1.8854     2.7381e+008     1.2892e+006           75100
v  TempK                    298.11          363.22          301.73          310.01
v  TurbVisc             3.048e-022      0.00017225     1.6738e-006     7.7785e-006
v  CourantNb            8.065e-006          1.0927         0.74744         0.96705
v  FourierNb             0.0025395               1         0.38804        0.079134
v  total_pressure      1.0061e+005     1.0148e+005     1.0129e+005      1.013e+005
v  Local Time Step          1e-006        0.002768      0.00012905      0.00034466

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.21          303.31          305.45
v  Yplus               0          3.1318         0.49176         0.28975


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.17513               2          1.1355          1.0462


 INSTANT    0.600000000E-03   TIME STEP NUMBER              60
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925044E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82544E-02 0.50220E+01
   Friction velocity        uk    :  0.82544E-02 0.50203E+01
   Dimensionless distance   yplus :  0.53072E-02 0.31093E+01
   Friction thermal sca.    tstar : -0.30370E+00 0.24071E+02
   Rough dim-less th. sca.  tplus :  0.37597E-02 0.22026E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        145 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16889E+00      11   0.64211E-05   0.64916E+02 0.27122E+03 
c  Velocity[X]                                      0.33841E+02 
c  Velocity[Y]                                      0.71392E+01 
c  Velocity[Z]                                      0.23936E+02 
c  Pressure     0.37730E-04      25   0.14621E-02   0.66007E-01 0.12285E+03 
c  k            0.10721E-03      14   0.18736E-03   0.83861E-03 0.51802E+03 
c  omega        0.27927E+07       1   0.63181E-06   0.53833E+09 0.51694E+01 
c  TempK        0.63757E+04       9   0.39835E-05   0.26761E+04 0.20563E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -6.2926e-007                           166
a  omega          
a  TempK          
a  Local Time Step     9.0376e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -26.51          24.097      -0.0053508     -0.00017551
v  Velocity[Y]             -15.728          18.043        0.021501        0.027904
v  Velocity[Z]             -27.099           11.51         -1.6016        -0.50914
v  ǁVelocityǁ        5.3795e-005          27.531            5.39          4.5647
v  Pressure                -709.07          149.57         -38.888          -23.57
v  k                   1.3019e-014          2.0398       0.0016856       0.0041517
v  omega                     1.994     2.7378e+008     1.2892e+006           75109
v  TempK                    298.11          363.21          301.86          310.17
v  TurbVisc             3.244e-022      0.00017346     1.6868e-006      7.844e-006
v  CourantNb           8.1704e-006          1.1065         0.74853          0.9677
v  FourierNb             0.0025392               1         0.38758        0.079286
v  total_pressure      1.0062e+005     1.0147e+005     1.0129e+005      1.013e+005
v  Local Time Step          1e-006       0.0030448      0.00012876      0.00034465

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.21          303.32          305.45
v  Yplus               0          3.1093         0.49437         0.29271


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.17566               2          1.1361           1.047


 INSTANT    0.610000000E-03   TIME STEP NUMBER              61
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924963E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78084E-02 0.49832E+01
   Friction velocity        uk    :  0.78084E-02 0.49815E+01
   Dimensionless distance   yplus :  0.50204E-02 0.30853E+01
   Friction thermal sca.    tstar : -0.30371E+00 0.24097E+02
   Rough dim-less th. sca.  tplus :  0.35565E-02 0.21856E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        143 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16925E+00      11   0.63482E-05   0.64024E+02 0.26869E+03 
c  Velocity[X]                                      0.33484E+02 
c  Velocity[Y]                                      0.69354E+01 
c  Velocity[Z]                                      0.23605E+02 
c  Pressure     0.40438E-04      26   0.14563E-02   0.70277E-01 0.14832E+03 
c  k            0.11067E-03      14   0.15944E-03   0.87048E-03 0.55391E+03 
c  omega        0.27927E+07       1   0.65771E-06   0.60042E+09 0.54532E+01 
c  TempK        0.63905E+04       9   0.38918E-05   0.26194E+04 0.21679E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -4.6232e-007                           170
a  omega          
a  TempK          
a  Local Time Step     8.9411e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -26.397          24.163      -0.0053823     4.2923e-005
v  Velocity[Y]             -15.646          17.678         0.02201        0.028544
v  Velocity[Z]             -26.997          11.054         -1.6066        -0.50895
v  ǁVelocityǁ        5.7242e-005          27.353          5.4211          4.5777
v  Pressure                -699.53          146.34         -38.215         -22.889
v  k                   1.4745e-014          2.1967       0.0017524       0.0042384
v  omega                    2.0938     2.7374e+008     1.2893e+006           75118
v  TempK                    298.12          363.21          301.99          310.32
v  TurbVisc            3.2929e-022      0.00017419     1.7018e-006     7.9142e-006
v  CourantNb           8.3303e-006          1.1184         0.74951         0.96824
v  FourierNb             0.0025387               1         0.38706        0.079365
v  total_pressure      1.0063e+005     1.0147e+005     1.0129e+005      1.013e+005
v  Local Time Step          1e-006       0.0033493      0.00012821      0.00034417

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15           363.2          303.32          305.45
v  Yplus               0          3.0853         0.49687         0.29564


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.15753               2          1.1366          1.0476


 INSTANT    0.620000000E-03   TIME STEP NUMBER              62
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924986E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78873E-02 0.49428E+01
   Friction velocity        uk    :  0.78873E-02 0.49411E+01
   Dimensionless distance   yplus :  0.50712E-02 0.30602E+01
   Friction thermal sca.    tstar : -0.29264E+00 0.24119E+02
   Rough dim-less th. sca.  tplus :  0.35924E-02 0.21679E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        136 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16960E+00      11   0.62804E-05   0.63188E+02 0.26630E+03 
c  Velocity[X]                                      0.33140E+02 
c  Velocity[Y]                                      0.67512E+01 
c  Velocity[Z]                                      0.23297E+02 
c  Pressure     0.42417E-04      25   0.14466E-02   0.73233E-01 0.16801E+03 
c  k            0.11422E-03      14   0.13636E-03   0.95773E-03 0.59329E+03 
c  omega        0.27927E+07       1   0.66888E-06   0.60212E+09 0.55149E+01 
c  TempK        0.64051E+04       9   0.38035E-05   0.25649E+04 0.22825E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.459e-007                           172
a  omega          
a  TempK          
a  Local Time Step     8.8596e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -26.352          24.225      -0.0054058      0.00026726
v  Velocity[Y]             -15.559          17.291        0.022518        0.029193
v  Velocity[Z]             -26.905          11.101         -1.6112        -0.50874
v  ǁVelocityǁ        4.4465e-005          27.158          5.4513          4.5905
v  Pressure                -689.53          144.35         -37.353         -22.021
v  k                   1.6439e-014          2.7385       0.0018241       0.0043245
v  omega                    2.1829      2.737e+008     1.2893e+006           75128
v  TempK                    298.13           363.2          302.12          310.45
v  TurbVisc            3.7294e-022      0.00017487     1.7185e-006     7.9872e-006
v  CourantNb           8.3252e-006          1.1287         0.75038          0.9687
v  FourierNb             0.0025385               1         0.38653        0.079403
v  total_pressure      1.0064e+005     1.0147e+005     1.0129e+005      1.013e+005
v  Local Time Step          1e-006       0.0036842       0.0001275      0.00034328

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15           363.2          303.33          305.45
v  Yplus               0          3.0602         0.49928         0.29852


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.14146               2          1.1369          1.0481


 INSTANT    0.630000000E-03   TIME STEP NUMBER              63
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924931E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78718E-02 0.49015E+01
   Friction velocity        uk    :  0.78718E-02 0.48998E+01
   Dimensionless distance   yplus :  0.56484E-02 0.30390E+01
   Friction thermal sca.    tstar : -0.27022E+00 0.24944E+02
   Rough dim-less th. sca.  tplus :  0.40014E-02 0.21528E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        139 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.16995E+00      11   0.61976E-05   0.62398E+02 0.26400E+03 
c  Velocity[X]                                      0.32810E+02 
c  Velocity[Y]                                      0.65771E+01 
c  Velocity[Z]                                      0.23011E+02 
c  Pressure     0.44494E-04      25   0.14664E-02   0.76316E-01 0.19216E+03 
c  k            0.11783E-03      14   0.11649E-03   0.97558E-03 0.63333E+03 
c  omega        0.27927E+07       1   0.67049E-06   0.58394E+09 0.54676E+01 
c  TempK        0.64194E+04       9   0.37223E-05   0.25124E+04 0.23986E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -4.2245e-007                           161
a  omega          
a  TempK          
a  Local Time Step     8.7898e-007                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -26.288          24.305      -0.0054203      0.00047701
v  Velocity[Y]             -15.509          16.896        0.023021        0.029839
v  Velocity[Z]             -26.823          11.132         -1.6154        -0.50854
v  ǁVelocityǁ        2.1992e-005          27.002          5.4806          4.6032
v  Pressure                -679.07          142.16         -36.286         -20.948
v  k                   1.2961e-014          2.8472       0.0019007       0.0044101
v  omega                    2.2467     2.7366e+008     1.2893e+006           75137
v  TempK                    298.13           363.2          302.27          310.58
v  TurbVisc            4.1561e-022       0.0001755     1.7367e-006     8.0629e-006
v  CourantNb           8.2066e-006          1.1377         0.75116         0.96907
v  FourierNb             0.0025388               1         0.38604        0.079409
v  total_pressure      1.0065e+005     1.0147e+005     1.0129e+005      1.013e+005
v  Local Time Step          1e-006       0.0040527      0.00012668        0.000342

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15           363.2          303.33          305.45
v  Yplus               0           3.039         0.50159         0.30136


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.20039               2          1.1372          1.0485


 INSTANT    0.640000000E-03   TIME STEP NUMBER              64
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924950E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54847E-02 0.48604E+01
   Friction velocity        uk    :  0.54847E-02 0.48588E+01
   Dimensionless distance   yplus :  0.39356E-02 0.30327E+01
   Friction thermal sca.    tstar : -0.23634E+00 0.24153E+02
   Rough dim-less th. sca.  tplus :  0.27880E-02 0.21483E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        134 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17029E+00      11   0.61382E-05   0.61684E+02 0.26179E+03 
c  Velocity[X]                                      0.32488E+02 
c  Velocity[Y]                                      0.64176E+01 
c  Velocity[Z]                                      0.22779E+02 
c  Pressure     0.46012E-04      25   0.14602E-02   0.78397E-01 0.21293E+03 
c  k            0.12154E-03      14   0.11389E-03   0.10756E-02 0.67366E+03 
c  omega        0.27927E+07       1   0.66828E-06   0.56994E+09 0.53948E+01 
c  TempK        0.64334E+04       9   0.36490E-05   0.24615E+04 0.25145E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -3.5476e-007                           157
a  omega          
a  TempK          
a  Local Time Step     8.7311e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -26.204          24.362      -0.0054253      0.00065243
v  Velocity[Y]             -15.587          16.726        0.023513         0.03048
v  Velocity[Z]             -26.749          11.142         -1.6192        -0.50835
v  ǁVelocityǁ        3.8337e-005          26.926          5.5091          4.6157
v  Pressure                -668.45          140.08          -35.06         -19.717
v  k                   1.9442e-015           3.078       0.0019824       0.0044956
v  omega                     2.309     2.7362e+008     1.2894e+006           75147
v  TempK                    298.14           363.2          302.41          310.69
v  TurbVisc            3.2768e-022      0.00017607     1.7565e-006      8.141e-006
v  CourantNb           8.2549e-006          1.1453         0.75187         0.96937
v  FourierNb             0.0025394               1         0.38557        0.079399
v  total_pressure      1.0066e+005     1.0147e+005     1.0129e+005     1.0131e+005
v  Local Time Step          1e-006       0.0044579       0.0001258      0.00034046

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.19          303.33          305.45
v  Yplus               0          3.0327         0.50381         0.30414


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.17844               2          1.1374          1.0488


 INSTANT    0.650000000E-03   TIME STEP NUMBER              65
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924903E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72621E-02 0.48484E+01
   Friction velocity        uk    :  0.72621E-02 0.48472E+01
   Dimensionless distance   yplus :  0.52109E-02 0.30270E+01
   Friction thermal sca.    tstar : -0.19066E+00 0.40515E+02
   Rough dim-less th. sca.  tplus :  0.36914E-02 0.21443E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        118 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17063E+00      11   0.60739E-05   0.61034E+02 0.25970E+03 
c  Velocity[X]                                      0.32185E+02 
c  Velocity[Y]                                      0.62713E+01 
c  Velocity[Z]                                      0.22578E+02 
c  Pressure     0.46744E-04      26   0.15131E-02   0.79116E-01 0.22539E+03 
c  k            0.12531E-03      14   0.13033E-03   0.12235E-02 0.71874E+03 
c  omega        0.27927E+07       1   0.66286E-06   0.55940E+09 0.53150E+01 
c  TempK        0.64471E+04       9   0.35803E-05   0.24120E+04 0.26284E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.3906e-007                           146
a  omega          
a  TempK          
a  Local Time Step     8.6827e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -26.098          24.397      -0.0054248      0.00081218
v  Velocity[Y]             -15.807          16.579        0.024003        0.031117
v  Velocity[Z]             -26.683          11.129         -1.6228        -0.50816
v  ǁVelocityǁ        4.1471e-005          26.858          5.5368           4.628
v  Pressure                -657.91          137.86         -33.749         -18.403
v  k                   9.7753e-015          2.8576       0.0020692       0.0045808
v  omega                     2.371     2.7359e+008     1.2894e+006           75157
v  TempK                    298.14          363.19          302.57          310.79
v  TurbVisc            4.9257e-023      0.00017659     1.7778e-006     8.2216e-006
v  CourantNb           7.6226e-006          1.1517         0.75252          0.9696
v  FourierNb             0.0025405               1         0.38514        0.079381
v  total_pressure      1.0067e+005     1.0146e+005     1.0129e+005     1.0131e+005
v  Local Time Step          1e-006       0.0049037      0.00012489       0.0003387

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.19          303.33          305.45
v  Yplus               0           3.027         0.50593         0.30688


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.22889               2          1.1377           1.049


 INSTANT    0.660000000E-03   TIME STEP NUMBER              66
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924935E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75802E-02 0.48393E+01
   Friction velocity        uk    :  0.75802E-02 0.48380E+01
   Dimensionless distance   yplus :  0.54392E-02 0.30218E+01
   Friction thermal sca.    tstar : -0.13309E+00 0.37498E+02
   Rough dim-less th. sca.  tplus :  0.38532E-02 0.21406E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        131 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17096E+00      11   0.60211E-05   0.60420E+02 0.25771E+03 
c  Velocity[X]                                      0.31895E+02 
c  Velocity[Y]                                      0.61316E+01 
c  Velocity[Z]                                      0.22393E+02 
c  Pressure     0.46734E-04      26   0.15440E-02   0.78582E-01 0.22987E+03 
c  k            0.12923E-03      14   0.15866E-03   0.13816E-02 0.76152E+03 
c  omega        0.27927E+07       1   0.65625E-06   0.53419E+09 0.52017E+01 
c  TempK        0.64606E+04       9   0.35212E-05   0.23637E+04 0.27384E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.0278e-007                           134
a  omega          
a  TempK          
a  Local Time Step     8.6469e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -25.974           24.41      -0.0054219      0.00096524
v  Velocity[Y]             -15.785          16.451        0.024501        0.031754
v  Velocity[Z]             -26.623          11.183          -1.626        -0.50795
v  ǁVelocityǁ        3.7657e-005          26.797          5.5637          4.6402
v  Pressure                -656.15          135.41          -32.41         -17.063
v  k                   9.0677e-015          2.9378       0.0021612        0.004666
v  omega                    2.4337     2.7355e+008     1.2894e+006           75167
v  TempK                    298.15          363.19          302.73          310.88
v  TurbVisc            2.4714e-022      0.00017706     1.8004e-006     8.3038e-006
v  CourantNb           8.3657e-006          1.1565         0.75312         0.96979
v  FourierNb             0.0025423               1         0.38475        0.079367
v  total_pressure      1.0067e+005     1.0146e+005     1.0129e+005     1.0131e+005
v  Local Time Step          1e-006       0.0053941      0.00012399      0.00033684

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.19          303.34          305.45
v  Yplus               0          3.0218         0.50796         0.30955


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.26951               2          1.1379          1.0492


 INSTANT    0.670000000E-03   TIME STEP NUMBER              67
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924913E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72424E-02 0.48284E+01
   Friction velocity        uk    :  0.72424E-02 0.48271E+01
   Dimensionless distance   yplus :  0.51898E-02 0.30169E+01
   Friction thermal sca.    tstar : -0.63471E-01 0.24185E+02
   Rough dim-less th. sca.  tplus :  0.36765E-02 0.21372E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        128 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17129E+00      11   0.59779E-05   0.59838E+02 0.25578E+03 
c  Velocity[X]                                      0.31601E+02 
c  Velocity[Y]                                      0.60029E+01 
c  Velocity[Z]                                      0.22234E+02 
c  Pressure     0.46218E-04      26   0.15197E-02   0.77207E-01 0.23374E+03 
c  k            0.13329E-03      14   0.17841E-03   0.15073E-02 0.80251E+03 
c  omega        0.27927E+07       1   0.64897E-06   0.50273E+09 0.50774E+01 
c  TempK        0.64738E+04       9   0.34719E-05   0.23163E+04 0.28428E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.1518e-007                           117
a  omega          
a  TempK          
a  Local Time Step     8.6209e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -25.834            24.4      -0.0054098       0.0011044
v  Velocity[Y]             -15.726           16.34        0.025004        0.032405
v  Velocity[Z]              -26.57          11.324          -1.629        -0.50772
v  ǁVelocityǁ        2.1696e-005          26.742          5.5899          4.6522
v  Pressure                -657.05          133.76         -31.039          -15.69
v  k                   7.7492e-016          3.6363       0.0022583       0.0047511
v  omega                    2.4974     2.7352e+008     1.2895e+006           75177
v  TempK                    298.15          363.19          302.89          310.97
v  TurbVisc            2.2925e-022      0.00017747     1.8244e-006     8.3871e-006
v  CourantNb           8.3203e-006            1.16         0.75368         0.96996
v  FourierNb             0.0025448               1         0.38439        0.079353
v  total_pressure      1.0067e+005     1.0146e+005     1.0129e+005     1.0131e+005
v  Local Time Step          1e-006       0.0059335      0.00012308      0.00033488

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.19          303.34          305.45
v  Yplus               0          3.0169         0.50989         0.31218


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.23749               2          1.1381          1.0493


 INSTANT    0.680000000E-03   TIME STEP NUMBER              68
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924926E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54667E-02 0.48160E+01
   Friction velocity        uk    :  0.54667E-02 0.48145E+01
   Dimensionless distance   yplus :  0.39104E-02 0.30127E+01
   Friction thermal sca.    tstar : -0.19117E-05 0.24193E+02
   Rough dim-less th. sca.  tplus :  0.27701E-02 0.21342E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        107 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17162E+00      11   0.59268E-05   0.59352E+02 0.25400E+03 
c  Velocity[X]                                      0.31340E+02 
c  Velocity[Y]                                      0.58872E+01 
c  Velocity[Z]                                      0.22125E+02 
c  Pressure     0.45872E-04      26   0.14764E-02   0.76125E-01 0.23662E+03 
c  k            0.13750E-03      14   0.17582E-03   0.15615E-02 0.83827E+03 
c  omega        0.27927E+07       1   0.64228E-06   0.49246E+09 0.49930E+01 
c  TempK        0.64869E+04       9   0.34285E-05   0.22697E+04 0.29399E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.4921e-007                           108
a  omega          
a  TempK          
a  Local Time Step     8.6013e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -25.681          24.369      -0.0053911       0.0012413
v  Velocity[Y]             -15.698          16.207        0.025513        0.033061
v  Velocity[Z]             -26.521          11.449         -1.6317         -0.5075
v  ǁVelocityǁ        1.1871e-005          26.692          5.6154          4.6641
v  Pressure                 -657.1          135.11         -29.653         -14.303
v  k                   3.2135e-016          4.2005       0.0023603       0.0048361
v  omega                    2.5619     2.7348e+008     1.2895e+006           75187
v  TempK                    298.15          363.19          303.06          311.05
v  TurbVisc            1.9557e-023      0.00017784     1.8494e-006      8.471e-006
v  CourantNb           8.5799e-006          1.1626         0.75419         0.97009
v  FourierNb             0.0025483               1         0.38406        0.079339
v  total_pressure      1.0067e+005     1.0146e+005      1.013e+005     1.0131e+005
v  Local Time Step          1e-006       0.0065268      0.00012219      0.00033284

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.18          303.34          305.45
v  Yplus               0          3.0127         0.51175         0.31475


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.14924               2          1.1383          1.0494


 INSTANT    0.690000000E-03   TIME STEP NUMBER              69
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924960E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41054E-02 0.48029E+01
   Friction velocity        uk    :  0.41054E-02 0.48014E+01
   Dimensionless distance   yplus :  0.29366E-02 0.30088E+01
   Friction thermal sca.    tstar : -0.26637E-05 0.24199E+02
   Rough dim-less th. sca.  tplus :  0.20803E-02 0.21315E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        116 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17195E+00      11   0.58938E-05   0.58900E+02 0.25222E+03 
c  Velocity[X]                                      0.31081E+02 
c  Velocity[Y]                                      0.57809E+01 
c  Velocity[Z]                                      0.22038E+02 
c  Pressure     0.45582E-04      26   0.15213E-02   0.75134E-01 0.24148E+03 
c  k            0.14177E-03      14   0.15219E-03   0.15687E-02 0.86419E+03 
c  omega        0.27927E+07       1   0.63497E-06   0.48334E+09 0.49009E+01 
c  TempK        0.64998E+04       9   0.33915E-05   0.22238E+04 0.30282E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.9352e-007                            97
a  omega          
a  TempK          
a  Local Time Step     8.5853e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -25.516          24.317      -0.0053735       0.0013616
v  Velocity[Y]             -15.833          16.056        0.026015        0.033721
v  Velocity[Z]             -26.477          11.554         -1.6342        -0.50727
v  ǁVelocityǁ        4.8689e-005          26.647          5.6403          4.6759
v  Pressure                -656.34          136.49         -28.244         -12.896
v  k                   2.8145e-015          4.5404       0.0024668       0.0049208
v  omega                    2.6275     2.7345e+008     1.2895e+006           75197
v  TempK                    298.15          363.18          303.23          311.12
v  TurbVisc            8.1212e-024      0.00017817     1.8756e-006     8.5557e-006
v  CourantNb           8.8882e-006          1.1648         0.75468         0.97021
v  FourierNb             0.0025528               1         0.38376        0.079323
v  total_pressure      1.0067e+005     1.0146e+005      1.013e+005     1.0131e+005
v  Local Time Step          1e-006       0.0071795      0.00012131      0.00033074

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.18          303.34          305.45
v  Yplus               0          3.0088         0.51354         0.31726


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.24539               2          1.1384          1.0495


 INSTANT    0.700000000E-03   TIME STEP NUMBER              70
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924857E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82140E-02 0.47898E+01
   Friction velocity        uk    :  0.82140E-02 0.47882E+01
   Dimensionless distance   yplus :  0.58939E-02 0.30053E+01
   Friction thermal sca.    tstar : -0.36986E-05 0.41905E+02
   Rough dim-less th. sca.  tplus :  0.41753E-02 0.21290E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        103 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17228E+00      11   0.58602E-05   0.58448E+02 0.25044E+03 
c  Velocity[X]                                      0.30811E+02 
c  Velocity[Y]                                      0.56778E+01 
c  Velocity[Z]                                      0.21960E+02 
c  Pressure     0.45322E-04      26   0.14903E-02   0.74200E-01 0.24310E+03 
c  k            0.14605E-03      14   0.12239E-03   0.15718E-02 0.88276E+03 
c  omega        0.27927E+07       1   0.62678E-06   0.46379E+09 0.47824E+01 
c  TempK        0.65124E+04       9   0.33604E-05   0.21784E+04 0.31063E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -3.4246e-007                            82
a  omega          
a  TempK          
a  Local Time Step      8.567e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -25.339          24.246      -0.0053497       0.0014619
v  Velocity[Y]             -15.949           15.89        0.026515        0.034378
v  Velocity[Z]             -26.436          11.636         -1.6364        -0.50702
v  ǁVelocityǁ        3.7351e-005          26.605          5.6645          4.6876
v  Pressure                -654.61           137.9         -26.829         -11.486
v  k                   2.6708e-015          4.7036       0.0025776       0.0050053
v  omega                    2.6939     2.7342e+008     1.2896e+006           75207
v  TempK                    298.15          363.18           303.4          311.19
v  TurbVisc            7.1307e-023      0.00017847     1.9028e-006     8.6395e-006
v  CourantNb           9.6668e-006          1.1673         0.75515         0.97031
v  FourierNb             0.0025585               1          0.3835        0.079301
v  total_pressure      1.0067e+005     1.0146e+005      1.013e+005     1.0131e+005
v  Local Time Step          1e-006       0.0078975      0.00012045      0.00032863

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.18          303.34          305.45
v  Yplus               0          3.0053         0.51526         0.31973


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.19095               2          1.1387          1.0496


 INSTANT    0.710000000E-03   TIME STEP NUMBER              71
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924848E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11557E-01 0.47771E+01
   Friction velocity        uk    :  0.11557E-01 0.47754E+01
   Dimensionless distance   yplus :  0.77093E-02 0.30022E+01
   Friction thermal sca.    tstar : -0.51111E-05 0.45934E+02
   Rough dim-less th. sca.  tplus :  0.54614E-02 0.21268E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        116 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17261E+00      11   0.58276E-05   0.57994E+02 0.24866E+03 
c  Velocity[X]                                      0.30539E+02 
c  Velocity[Y]                                      0.55787E+01 
c  Velocity[Z]                                      0.21876E+02 
c  Pressure     0.45200E-04      27   0.14694E-02   0.73490E-01 0.24430E+03 
c  k            0.15032E-03      14   0.10872E-03   0.15840E-02 0.89302E+03 
c  omega        0.27927E+07       1   0.62037E-06   0.45263E+09 0.46947E+01 
c  TempK        0.65250E+04       9   0.33324E-05   0.21336E+04 0.31732E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -3.4513e-007                            66
a  omega          
a  TempK          
a  Local Time Step     8.5474e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -25.15          24.199       -0.005318       0.0015465
v  Velocity[Y]             -15.891          15.709        0.027009        0.035035
v  Velocity[Z]             -26.398          11.695         -1.6385        -0.50676
v  ǁVelocityǁ         0.00011999          26.567          5.6882          4.6992
v  Pressure                -651.94          139.32         -25.408         -10.067
v  k                   4.2251e-015          4.7638       0.0026922       0.0050893
v  omega                    2.7614     2.7339e+008     1.2896e+006           75217
v  TempK                    298.15          363.18          303.58          311.25
v  TurbVisc             6.733e-023      0.00017874     1.9307e-006     8.7223e-006
v  CourantNb           9.2377e-006          1.1699          0.7556         0.97041
v  FourierNb             0.0025654               1         0.38325        0.079275
v  total_pressure      1.0067e+005     1.0146e+005      1.013e+005     1.0131e+005
v  Local Time Step          1e-006       0.0086872       0.0001196      0.00032654

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.18          303.34          305.45
v  Yplus               0          3.0022         0.51691         0.32214


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.24429               2          1.1389          1.0497


 INSTANT    0.720000000E-03   TIME STEP NUMBER              72
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924828E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13201E-01 0.47655E+01
   Friction velocity        uk    :  0.13201E-01 0.47637E+01
   Dimensionless distance   yplus :  0.84887E-02 0.29994E+01
   Friction thermal sca.    tstar : -0.70082E-05 0.34848E+02
   Rough dim-less th. sca.  tplus :  0.60134E-02 0.21248E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for        114 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17294E+00      11   0.57834E-05   0.57559E+02 0.24689E+03 
c  Velocity[X]                                      0.30284E+02 
c  Velocity[Y]                                      0.54807E+01 
c  Velocity[Z]                                      0.21794E+02 
c  Pressure     0.44928E-04      26   0.14583E-02   0.72538E-01 0.24565E+03 
c  k            0.15460E-03      14   0.10531E-03   0.16212E-02 0.89957E+03 
c  omega        0.27927E+07       1   0.61296E-06   0.42447E+09 0.45705E+01 
c  TempK        0.65374E+04       9   0.33093E-05   0.20893E+04 0.32281E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.2682e-007                            52
a  omega          
a  TempK          
a  Local Time Step     8.5215e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -24.952          24.176      -0.0052775        0.001623
v  Velocity[Y]             -15.809          15.518        0.027503         0.03569
v  Velocity[Z]             -26.362           12.98         -1.6404        -0.50651
v  ǁVelocityǁ         0.00011924          26.531          5.7113          4.7108
v  Pressure                -648.48          140.75         -23.982         -8.6466
v  k                   4.4655e-015          4.7868       0.0028103       0.0051729
v  omega                    2.8303     2.7337e+008     1.2896e+006           75228
v  TempK                    298.15          363.18          303.76          311.31
v  TurbVisc            1.0653e-022      0.00017898     1.9594e-006     8.8037e-006
v  CourantNb           8.5286e-006          1.1735         0.75602         0.97049
v  FourierNb             0.0025739               1         0.38302        0.079244
v  total_pressure      1.0068e+005     1.0147e+005      1.013e+005     1.0132e+005
v  Local Time Step          1e-006       0.0095559      0.00011878      0.00032447

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.18          303.34          305.45
v  Yplus               0          2.9994         0.51848          0.3245


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.19055               2           1.139          1.0497


 INSTANT    0.730000000E-03   TIME STEP NUMBER              73
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924826E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12796E-01 0.47552E+01
   Friction velocity        uk    :  0.12796E-01 0.47533E+01
   Dimensionless distance   yplus :  0.91814E-02 0.29968E+01
   Friction thermal sca.    tstar : -0.93672E-05 0.48635E+02
   Rough dim-less th. sca.  tplus :  0.65042E-02 0.21229E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         96 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17327E+00      11   0.57537E-05   0.57165E+02 0.24512E+03 
c  Velocity[X]                                      0.30037E+02 
c  Velocity[Y]                                      0.53944E+01 
c  Velocity[Z]                                      0.21734E+02 
c  Pressure     0.44586E-04      26   0.14658E-02   0.71468E-01 0.24848E+03 
c  k            0.15889E-03      14   0.11372E-03   0.16975E-02 0.90376E+03 
c  omega        0.27926E+07       1   0.60762E-06   0.41999E+09 0.45104E+01 
c  TempK        0.65497E+04       9   0.32864E-05   0.20456E+04 0.32704E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.0157e-007                            39
a  omega          
a  TempK          
a  Local Time Step     8.4905e-007        0.010512             2            18


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -24.819          24.135      -0.0052337       0.0016804
v  Velocity[Y]             -15.787          15.596        0.027992        0.036346
v  Velocity[Z]             -26.329          13.353         -1.6421        -0.50625
v  ǁVelocityǁ         0.00010686          26.497          5.7338          4.7222
v  Pressure                -645.48          142.22         -22.541         -7.2153
v  k                   6.0719e-016          4.7502       0.0029316       0.0052558
v  omega                    2.9007     2.7334e+008     1.2896e+006           75238
v  TempK                    298.15          363.18          303.94          311.36
v  TurbVisc             1.129e-022       0.0001792     1.9886e-006     8.8834e-006
v  CourantNb           7.7889e-006          1.1778         0.75641         0.97056
v  FourierNb             0.0025841               1         0.38281        0.079206
v  total_pressure      1.0068e+005     1.0147e+005      1.013e+005     1.0132e+005
v  Local Time Step          1e-006            0.01      0.00011799      0.00032243

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.18          303.35          305.45
v  Yplus               0          2.9968         0.51998         0.32679


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.19728               2          1.1392          1.0498


 INSTANT    0.740000000E-03   TIME STEP NUMBER              74
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924721E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12091E-01 0.47466E+01
   Friction velocity        uk    :  0.12091E-01 0.47447E+01
   Dimensionless distance   yplus :  0.86756E-02 0.29944E+01
   Friction thermal sca.    tstar : -0.12116E-04 0.42855E+02
   Rough dim-less th. sca.  tplus :  0.61459E-02 0.21212E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         99 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17360E+00      11   0.57334E-05   0.56797E+02 0.24335E+03 
c  Velocity[X]                                      0.29794E+02 
c  Velocity[Y]                                      0.53117E+01 
c  Velocity[Z]                                      0.21691E+02 
c  Pressure     0.44356E-04      27   0.14560E-02   0.70587E-01 0.24850E+03 
c  k            0.16321E-03      14   0.13790E-03   0.18006E-02 0.90476E+03 
c  omega        0.27926E+07       1   0.60191E-06   0.40593E+09 0.44233E+01 
c  TempK        0.65620E+04       9   0.32642E-05   0.20025E+04 0.32998E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -7.9937e-008                            30
a  omega          
a  TempK          
a  Local Time Step     8.4526e-007           0.011             2            14


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -24.679          24.075      -0.0051966       0.0017122
v  Velocity[Y]             -15.917          15.551        0.028475           0.037
v  Velocity[Z]             -26.297          13.411         -1.6437        -0.50599
v  ǁVelocityǁ        9.4806e-005          26.465          5.7557          4.7336
v  Pressure                -644.34          143.69         -21.104         -5.7903
v  k                   6.0598e-015          4.6539       0.0030558       0.0053382
v  omega                    2.9727     2.7332e+008     1.2897e+006           75248
v  TempK                    298.15          363.18          304.12          311.41
v  TurbVisc            1.5351e-023       0.0001794     2.0182e-006     8.9611e-006
v  CourantNb           7.8983e-006          1.1831         0.75679         0.97062
v  FourierNb             0.0025965               1         0.38262        0.079156
v  total_pressure      1.0068e+005     1.0147e+005      1.013e+005     1.0132e+005
v  Local Time Step          1e-006            0.01      0.00011723      0.00032042

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.18          303.35          305.45
v  Yplus               0          2.9944         0.52141         0.32904


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.16752               2          1.1394          1.0498


 INSTANT    0.750000000E-03   TIME STEP NUMBER              75
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924787E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11364E-01 0.47398E+01
   Friction velocity        uk    :  0.11364E-01 0.47377E+01
   Dimensionless distance   yplus :  0.81544E-02 0.29922E+01
   Friction thermal sca.    tstar : -0.15267E-04 0.29944E+02
   Rough dim-less th. sca.  tplus :  0.57766E-02 0.21197E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         91 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17394E+00      11   0.56989E-05   0.56447E+02 0.24156E+03 
c  Velocity[X]                                      0.29563E+02 
c  Velocity[Y]                                      0.52316E+01 
c  Velocity[Z]                                      0.21653E+02 
c  Pressure     0.43671E-04      25   0.14629E-02   0.68997E-01 0.24395E+03 
c  k            0.16760E-03      14   0.17776E-03   0.19479E-02 0.90373E+03 
c  omega        0.27926E+07       1   0.59712E-06   0.41472E+09 0.43997E+01 
c  TempK        0.65742E+04       9   0.32419E-05   0.19602E+04 0.33164E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -3.1724e-008                            26
a  omega          
a  TempK          
a  Local Time Step     8.4114e-007           0.011             2            12


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -24.529          23.997      -0.0051704       0.0017109
v  Velocity[Y]             -16.041          15.525        0.028951        0.037647
v  Velocity[Z]             -26.266           13.44         -1.6452        -0.50572
v  ǁVelocityǁ        8.6705e-005          26.435          5.7772           4.745
v  Pressure                -643.72          145.14         -19.703         -4.4059
v  k                   3.2441e-015          4.5347       0.0031825       0.0054199
v  omega                    3.0466      2.733e+008     1.2897e+006           75259
v  TempK                    298.15          363.18           304.3          311.46
v  TurbVisc            1.5293e-022      0.00017958      2.048e-006     9.0363e-006
v  CourantNb           8.1686e-006          1.1889         0.75715         0.97069
v  FourierNb             0.0026111               1         0.38244        0.079096
v  total_pressure      1.0068e+005     1.0147e+005     1.0131e+005     1.0132e+005
v  Local Time Step          1e-006            0.01      0.00011649      0.00031845

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.18          303.35          305.45
v  Yplus               0          2.9922         0.52277         0.33123


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.20715               2          1.1396          1.0498


 INSTANT    0.760000000E-03   TIME STEP NUMBER              76
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924724E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10839E-01 0.47348E+01
   Friction velocity        uk    :  0.10839E-01 0.47326E+01
   Dimensionless distance   yplus :  0.76207E-02 0.29901E+01
   Friction thermal sca.    tstar : -0.18690E-04 0.35886E+02
   Rough dim-less th. sca.  tplus :  0.53985E-02 0.21182E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         95 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17428E+00      11   0.56690E-05   0.56103E+02 0.23974E+03 
c  Velocity[X]                                      0.29338E+02 
c  Velocity[Y]                                      0.51571E+01 
c  Velocity[Z]                                      0.21608E+02 
c  Pressure     0.43127E-04      26   0.14707E-02   0.67651E-01 0.24076E+03 
c  k            0.17208E-03      14   0.23083E-03   0.21250E-02 0.90058E+03 
c  omega        0.27926E+07       1   0.59132E-06   0.38641E+09 0.43118E+01 
c  TempK        0.65863E+04       9   0.32174E-05   0.19187E+04 0.33205E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.6003e-008                            21
a  omega          
a  TempK          
a  Local Time Step     8.3695e-007           0.011             2            10


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -24.369          23.903      -0.0051516       0.0016781
v  Velocity[Y]             -15.996          15.493        0.029429        0.038292
v  Velocity[Z]             -26.237          13.449         -1.6466        -0.50545
v  ǁVelocityǁ        8.0337e-005          26.406          5.7982          4.7563
v  Pressure                -641.83          146.59         -18.322         -3.0424
v  k                   1.0957e-014          4.4041       0.0033113        0.005501
v  omega                    3.1228     2.7328e+008     1.2897e+006           75269
v  TempK                    298.15          363.18          304.48          311.51
v  TurbVisc            8.2293e-023      0.00017974     2.0778e-006     9.1089e-006
v  CourantNb            8.523e-006          1.1948         0.75749         0.97075
v  FourierNb             0.0026284               1         0.38228        0.079028
v  total_pressure      1.0068e+005     1.0147e+005     1.0131e+005     1.0132e+005
v  Local Time Step          1e-006            0.01      0.00011578      0.00031657

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.18          303.35          305.45
v  Yplus               0          2.9901         0.52407         0.33336


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.24938               2          1.1398          1.0498


 INSTANT    0.770000000E-03   TIME STEP NUMBER              77
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924696E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10415E-01 0.47313E+01
   Friction velocity        uk    :  0.10415E-01 0.47290E+01
   Dimensionless distance   yplus :  0.66583E-02 0.29882E+01
   Friction thermal sca.    tstar : -0.22231E-04 0.51256E+02
   Rough dim-less th. sca.  tplus :  0.47168E-02 0.21169E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         90 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17462E+00      11   0.56516E-05   0.55787E+02 0.23791E+03 
c  Velocity[X]                                      0.29115E+02 
c  Velocity[Y]                                      0.50919E+01 
c  Velocity[Z]                                      0.21580E+02 
c  Pressure     0.42475E-04      26   0.14583E-02   0.66154E-01 0.23805E+03 
c  k            0.17666E-03      14   0.23461E-03   0.22768E-02 0.89295E+03 
c  omega        0.27926E+07       1   0.58570E-06   0.36524E+09 0.41784E+01 
c  TempK        0.65984E+04       9   0.31900E-05   0.18782E+04 0.33124E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.298e-009                            19
a  omega          
a  TempK          
a  Local Time Step     8.3265e-007           0.011             2            10


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -24.2          23.793      -0.0051401       0.0016225
v  Velocity[Y]             -15.977          15.585         0.02991         0.03894
v  Velocity[Z]             -26.208          13.389         -1.6478        -0.50518
v  ǁVelocityǁ        6.9501e-005          26.378          5.8187          4.7676
v  Pressure                 -638.6          148.02         -16.959         -1.7002
v  k                   3.7276e-016          4.5798       0.0034419       0.0055814
v  omega                    3.2014     2.7326e+008     1.2897e+006           75279
v  TempK                    298.14          363.18          304.66          311.55
v  TurbVisc            2.7786e-022       0.0001799     2.1075e-006     9.1789e-006
v  CourantNb           8.6758e-006           1.201         0.75781          0.9708
v  FourierNb             0.0026485               1         0.38214        0.078952
v  total_pressure      1.0069e+005     1.0147e+005     1.0131e+005     1.0132e+005
v  Local Time Step          1e-006            0.01       0.0001151      0.00031476

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.18          303.35          305.45
v  Yplus               0          2.9882         0.52531         0.33545


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.32099               2            1.14          1.0498


 INSTANT    0.780000000E-03   TIME STEP NUMBER              78
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924665E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99060E-02 0.47292E+01
   Friction velocity        uk    :  0.99060E-02 0.47268E+01
   Dimensionless distance   yplus :  0.68587E-02 0.29864E+01
   Friction thermal sca.    tstar : -0.25656E-04 0.35932E+02
   Rough dim-less th. sca.  tplus :  0.48588E-02 0.21156E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         84 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17497E+00      11   0.56370E-05   0.55455E+02 0.23601E+03 
c  Velocity[X]                                      0.28884E+02 
c  Velocity[Y]                                      0.50378E+01 
c  Velocity[Z]                                      0.21533E+02 
c  Pressure     0.41783E-04      26   0.14597E-02   0.64603E-01 0.23285E+03 
c  k            0.18134E-03      14   0.23620E-03   0.24234E-02 0.88362E+03 
c  omega        0.27926E+07       1   0.58233E-06   0.36975E+09 0.41551E+01 
c  TempK        0.66105E+04       9   0.31589E-05   0.18386E+04 0.32928E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -3.3433e-009                            16
a  omega          
a  TempK          
a  Local Time Step     8.2836e-007           0.011             2             6


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -24.024           23.67       -0.005132       0.0015585
v  Velocity[Y]             -16.021          15.614        0.030391        0.039588
v  Velocity[Z]              -26.18          13.244          -1.649         -0.5049
v  ǁVelocityǁ        2.9235e-005           26.35          5.8389          4.7788
v  Pressure                -635.67          149.43         -15.631        -0.39477
v  k                   1.0861e-014          5.3577        0.003574        0.005661
v  omega                    3.2825     2.7325e+008     1.2897e+006           75290
v  TempK                    298.14          363.18          304.84          311.59
v  TurbVisc            9.4529e-024      0.00018004     2.1371e-006      9.246e-006
v  CourantNb           8.6256e-006          1.2072         0.75813         0.97086
v  FourierNb             0.0026719               1           0.382        0.078865
v  total_pressure      1.0069e+005     1.0147e+005     1.0131e+005     1.0132e+005
v  Local Time Step          1e-006            0.01      0.00011445        0.000313

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.18          303.35          305.45
v  Yplus               0          2.9864         0.52649         0.33749


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.24099               2          1.1401          1.0497


 INSTANT    0.790000000E-03   TIME STEP NUMBER              79
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924672E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63387E-02 0.47282E+01
   Friction velocity        uk    :  0.63387E-02 0.47256E+01
   Dimensionless distance   yplus :  0.45483E-02 0.29847E+01
   Friction thermal sca.    tstar : -0.28667E-04 0.24753E+02
   Rough dim-less th. sca.  tplus :  0.32221E-02 0.21143E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         87 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17532E+00      11   0.56034E-05   0.55134E+02 0.23408E+03 
c  Velocity[X]                                      0.28664E+02 
c  Velocity[Y]                                      0.49845E+01 
c  Velocity[Z]                                      0.21485E+02 
c  Pressure     0.41379E-04      25   0.14526E-02   0.63502E-01 0.22827E+03 
c  k            0.18612E-03      13   0.23458E-03   0.25645E-02 0.87289E+03 
c  omega        0.27926E+07       1   0.57807E-06   0.35051E+09 0.40650E+01 
c  TempK        0.66226E+04       9   0.31240E-05   0.18002E+04 0.32627E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.0528e-009                            14
a  omega          
a  TempK          
a  Local Time Step     8.2413e-007           0.011             2             5


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -23.842          23.591      -0.0051306       0.0014798
v  Velocity[Y]             -16.239          15.447        0.030861        0.040228
v  Velocity[Z]             -26.152          13.056           -1.65        -0.50464
v  ǁVelocityǁ        8.4146e-005          26.324          5.8586            4.79
v  Pressure                -633.53          150.82         -14.332         0.87881
v  k                   1.0956e-014          6.0355       0.0037074       0.0057399
v  omega                    3.3661     2.7323e+008     1.2898e+006           75300
v  TempK                    298.15          363.17          305.02          311.64
v  TurbVisc            2.7365e-022      0.00018017     2.1665e-006     9.3101e-006
v  CourantNb           1.0071e-005          1.2134         0.75844         0.97092
v  FourierNb             0.0026993               1         0.38187        0.078767
v  total_pressure      1.0069e+005     1.0148e+005     1.0131e+005     1.0133e+005
v  Local Time Step          1e-006            0.01      0.00011383      0.00031131

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.18          303.35          305.45
v  Yplus               0          2.9847         0.52763         0.33947


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.30459               2          1.1403          1.0497


 INSTANT    0.800000000E-03   TIME STEP NUMBER              80
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924627E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10665E-01 0.47279E+01
   Friction velocity        uk    :  0.10665E-01 0.47252E+01
   Dimensionless distance   yplus :  0.76524E-02 0.29830E+01
   Friction thermal sca.    tstar : -0.30860E-04 0.24225E+02
   Rough dim-less th. sca.  tplus :  0.54210E-02 0.21132E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         72 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17567E+00      11   0.55880E-05   0.54822E+02 0.23214E+03 
c  Velocity[X]                                      0.28445E+02 
c  Velocity[Y]                                      0.49383E+01 
c  Velocity[Z]                                      0.21439E+02 
c  Pressure     0.40784E-04      26   0.14576E-02   0.62115E-01 0.22329E+03 
c  k            0.19099E-03      13   0.22922E-03   0.26425E-02 0.85988E+03 
c  omega        0.27926E+07       1   0.57539E-06   0.37625E+09 0.40967E+01 
c  TempK        0.66346E+04       9   0.30847E-05   0.17629E+04 0.32229E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.2053e-010                            11
a  omega          
a  TempK          
a  Local Time Step     8.2008e-007           0.011             2             5


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -23.654          23.513      -0.0051327       0.0013856
v  Velocity[Y]             -16.411          15.444        0.031328         0.04086
v  Velocity[Z]             -26.125          12.871          -1.651        -0.50436
v  ǁVelocityǁ        8.5869e-005          26.298          5.8779          4.8011
v  Pressure                -631.43          152.19         -13.064          2.1195
v  k                    1.035e-014          6.6079       0.0038418       0.0058181
v  omega                    3.4522     2.7322e+008     1.2898e+006           75311
v  TempK                    298.14          363.17          305.19          311.68
v  TurbVisc            2.7603e-022       0.0001803     2.1955e-006     9.3713e-006
v  CourantNb            1.184e-005          1.2194         0.75873         0.97098
v  FourierNb              0.002731               1         0.38174        0.078655
v  total_pressure      1.0069e+005     1.0148e+005     1.0131e+005     1.0133e+005
v  Local Time Step          1e-006            0.01      0.00011322      0.00030967

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.35          305.45
v  Yplus               0           2.983         0.52872         0.34142


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.18806               2          1.1405          1.0496


 INSTANT    0.810000000E-03   TIME STEP NUMBER              81
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924740E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11428E-01 0.47280E+01
   Friction velocity        uk    :  0.11428E-01 0.47253E+01
   Dimensionless distance   yplus :  0.82004E-02 0.29815E+01
   Friction thermal sca.    tstar : -0.32999E-04 0.24225E+02
   Rough dim-less th. sca.  tplus :  0.58092E-02 0.21121E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         83 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17603E+00      11   0.55559E-05   0.54517E+02 0.23020E+03 
c  Velocity[X]                                      0.28228E+02 
c  Velocity[Y]                                      0.48922E+01 
c  Velocity[Z]                                      0.21397E+02 
c  Pressure     0.40381E-04      25   0.14597E-02   0.61034E-01 0.21749E+03 
c  k            0.19591E-03      13   0.22419E-03   0.26099E-02 0.84253E+03 
c  omega        0.27926E+07       1   0.56996E-06   0.33673E+09 0.39501E+01 
c  TempK        0.66467E+04       9   0.30403E-05   0.17269E+04 0.31746E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -8.6003e-011                             8
a  omega          
a  TempK          
a  Local Time Step     8.1635e-007           0.011             2             4


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -23.464          23.421       -0.005137        0.001288
v  Velocity[Y]             -16.423           15.52        0.031793        0.041483
v  Velocity[Z]             -26.099          12.716          -1.652        -0.50409
v  ǁVelocityǁ         0.00011414          26.273          5.8969          4.8123
v  Pressure                -629.26          153.52         -11.831          3.3248
v  k                   5.8826e-015          7.0808       0.0039771       0.0058956
v  omega                    3.5408     2.7321e+008     1.2898e+006           75322
v  TempK                    298.14          363.17          305.37          311.72
v  TurbVisc            2.6076e-022      0.00018042     2.2242e-006     9.4298e-006
v  CourantNb           1.2197e-005           1.225         0.75901         0.97102
v  FourierNb             0.0027672               1         0.38163        0.078534
v  total_pressure       1.007e+005     1.0148e+005     1.0131e+005     1.0133e+005
v  Local Time Step          1e-006            0.01      0.00011264      0.00030808

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.35          305.45
v  Yplus               0          2.9815         0.52976         0.34332


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.269               2          1.1406          1.0496


 INSTANT    0.820000000E-03   TIME STEP NUMBER              82
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924654E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12407E-01 0.47283E+01
   Friction velocity        uk    :  0.12407E-01 0.47254E+01
   Dimensionless distance   yplus :  0.89026E-02 0.29801E+01
   Friction thermal sca.    tstar : -0.38046E-04 0.28821E+02
   Rough dim-less th. sca.  tplus :  0.63067E-02 0.21111E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         69 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17639E+00      11   0.55331E-05   0.54230E+02 0.22827E+03 
c  Velocity[X]                                      0.28021E+02 
c  Velocity[Y]                                      0.48506E+01 
c  Velocity[Z]                                      0.21359E+02 
c  Pressure     0.40189E-04      27   0.14564E-02   0.60286E-01 0.21431E+03 
c  k            0.20079E-03      13   0.19410E-03   0.24323E-02 0.81827E+03 
c  omega        0.27926E+07       1   0.56554E-06   0.32333E+09 0.38706E+01 
c  TempK        0.66588E+04       9   0.29923E-05   0.16920E+04 0.31190E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -5.2135e-012                             6
a  omega          
a  TempK          
a  Local Time Step     8.1292e-007           0.011             2             3


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -23.337          23.316      -0.0051383       0.0011853
v  Velocity[Y]             -16.474          15.678        0.032263          0.0421
v  Velocity[Z]             -26.074          12.595         -1.6529        -0.50382
v  ǁVelocityǁ        9.0696e-005          26.248          5.9156          4.8234
v  Pressure                -626.64          154.85         -10.618          4.5048
v  k                   8.8612e-015          7.4554       0.0041128       0.0059726
v  omega                    3.6318      2.732e+008     1.2898e+006           75332
v  TempK                    298.14          363.17          305.54          311.76
v  TurbVisc            1.4863e-022      0.00018054     2.2525e-006     9.4855e-006
v  CourantNb            1.193e-005          1.2301         0.75929         0.97107
v  FourierNb             0.0028148               1         0.38151        0.078404
v  total_pressure       1.007e+005     1.0148e+005     1.0131e+005     1.0133e+005
v  Local Time Step          1e-006            0.01      0.00011208      0.00030655

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.35          305.45
v  Yplus               0          2.9801         0.53076         0.34517


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.29842               2          1.1408          1.0495


 INSTANT    0.830000000E-03   TIME STEP NUMBER              83
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924724E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11198E-01 0.47286E+01
   Friction velocity        uk    :  0.11198E-01 0.47256E+01
   Dimensionless distance   yplus :  0.80348E-02 0.29786E+01
   Friction thermal sca.    tstar : -0.43296E-04 0.53808E+02
   Rough dim-less th. sca.  tplus :  0.56919E-02 0.21101E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         73 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17676E+00      11   0.55225E-05   0.53956E+02 0.22635E+03 
c  Velocity[X]                                      0.27819E+02 
c  Velocity[Y]                                      0.48206E+01 
c  Velocity[Z]                                      0.21317E+02 
c  Pressure     0.39892E-04      26   0.14459E-02   0.59397E-01 0.20791E+03 
c  k            0.20561E-03      13   0.16042E-03   0.22608E-02 0.79180E+03 
c  omega        0.27926E+07       1   0.56256E-06   0.33148E+09 0.38531E+01 
c  TempK        0.66709E+04       9   0.29399E-05   0.16585E+04 0.30573E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -7.9473e-013                             3
a  omega          
a  TempK          
a  Local Time Step     8.0968e-007           0.011             2             3


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -23.194          23.198      -0.0051286        0.001079
v  Velocity[Y]             -16.563          15.707        0.032732        0.042709
v  Velocity[Z]             -26.049          12.493         -1.6537        -0.50355
v  ǁVelocityǁ        9.1228e-005          26.224          5.9339          4.8345
v  Pressure                -623.66          156.12         -9.4486          5.6396
v  k                   6.9053e-015          7.7376       0.0042491        0.006049
v  omega                    3.7254     2.7319e+008     1.2898e+006           75343
v  TempK                    298.14          363.17           305.7           311.8
v  TurbVisc            2.2326e-022      0.00018065     2.2802e-006     9.5384e-006
v  CourantNb           1.3891e-005          1.2351         0.75956         0.97113
v  FourierNb             0.0028813               1         0.38141        0.078263
v  total_pressure       1.007e+005     1.0148e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006            0.01      0.00011153      0.00030508

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.35          305.45
v  Yplus               0          2.9786         0.53173         0.34699


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.22431               2           1.141          1.0494


 INSTANT    0.840000000E-03   TIME STEP NUMBER              84
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924669E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11256E-01 0.47289E+01
   Friction velocity        uk    :  0.11256E-01 0.47258E+01
   Dimensionless distance   yplus :  0.80766E-02 0.29773E+01
   Friction thermal sca.    tstar : -0.48722E-04 0.39725E+02
   Rough dim-less th. sca.  tplus :  0.57215E-02 0.21091E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         57 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17713E+00      11   0.55037E-05   0.53673E+02 0.22443E+03 
c  Velocity[X]                                      0.27602E+02 
c  Velocity[Y]                                      0.47877E+01 
c  Velocity[Z]                                      0.21284E+02 
c  Pressure     0.39344E-04      25   0.14680E-02   0.58153E-01 0.20299E+03 
c  k            0.21032E-03      13   0.13564E-03   0.21021E-02 0.76110E+03 
c  omega        0.27926E+07       1   0.55911E-06   0.31927E+09 0.37793E+01 
c  TempK        0.66831E+04       9   0.28839E-05   0.16261E+04 0.29908E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.1715e-015                             1
a  omega          
a  TempK          
a  Local Time Step     8.0659e-007           0.011             2             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -23.037          23.069       -0.005126      0.00095962
v  Velocity[Y]             -17.019          15.605        0.033191        0.043312
v  Velocity[Z]             -26.025          12.381         -1.6545        -0.50327
v  ǁVelocityǁ         0.00012493          26.201          5.9519          4.8455
v  Pressure                -620.29          157.39         -8.3036          6.7486
v  k                   2.1715e-015          7.9402       0.0043858       0.0061252
v  omega                    3.8129     2.7318e+008     1.2898e+006           75353
v  TempK                    298.14          363.17          305.87          311.83
v  TurbVisc            1.7398e-022      0.00018075     2.3078e-006     9.5894e-006
v  CourantNb           1.9049e-005          1.2398         0.75983         0.97118
v  FourierNb             0.0029661               1          0.3813        0.078115
v  total_pressure       1.007e+005     1.0148e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006            0.01        0.000111      0.00030362

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.35          305.45
v  Yplus               0          2.9773         0.53265         0.34876


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.33388               2          1.1411          1.0493


 INSTANT    0.850000000E-03   TIME STEP NUMBER              85
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924761E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13201E-01 0.47294E+01
   Friction velocity        uk    :  0.13201E-01 0.47262E+01
   Dimensionless distance   yplus :  0.94724E-02 0.29760E+01
   Friction thermal sca.    tstar : -0.54293E-04 0.31208E+02
   Rough dim-less th. sca.  tplus :  0.67103E-02 0.21082E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         65 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17751E+00      11   0.54833E-05   0.53389E+02 0.22251E+03 
c  Velocity[X]                                      0.27396E+02 
c  Velocity[Y]                                      0.47642E+01 
c  Velocity[Z]                                      0.21229E+02 
c  Pressure     0.38904E-04      25   0.14610E-02   0.57092E-01 0.19469E+03 
c  k            0.21493E-03      13   0.12495E-03   0.19936E-02 0.73076E+03 
c  omega        0.27926E+07       1   0.55609E-06   0.32729E+09 0.37656E+01 
c  TempK        0.66952E+04       9   0.28247E-05   0.15950E+04 0.29209E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.0385e-007           0.011             2             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.868           22.93      -0.0051206      0.00082741
v  Velocity[Y]             -16.858          15.541        0.033653        0.043914
v  Velocity[Z]             -26.002          12.251         -1.6552        -0.50301
v  ǁVelocityǁ         0.00014232          26.179          5.9696          4.8565
v  Pressure                -616.59           158.6         -7.2081          7.8086
v  k                   7.0286e-015          8.0789        0.004523       0.0062011
v  omega                    3.8846     2.7318e+008     1.2898e+006           75364
v  TempK                    298.14          363.17          306.03          311.87
v  TurbVisc            5.4713e-023      0.00018493      2.335e-006      9.638e-006
v  CourantNb           2.4137e-005           1.244         0.76008         0.97123
v  FourierNb             0.0030376               1         0.38121         0.07796
v  total_pressure      1.0071e+005     1.0148e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006            0.01      0.00011049      0.00030219

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.35          305.45
v  Yplus               0           2.976         0.53354         0.35049


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.28837               2          1.1413          1.0492


 INSTANT    0.860000000E-03   TIME STEP NUMBER              86
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924718E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14055E-01 0.47298E+01
   Friction velocity        uk    :  0.14055E-01 0.47265E+01
   Dimensionless distance   yplus :  0.10085E-01 0.29748E+01
   Friction thermal sca.    tstar : -0.59965E-04 0.34152E+02
   Rough dim-less th. sca.  tplus :  0.71446E-02 0.21074E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         68 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17788E+00      11   0.54659E-05   0.53095E+02 0.22054E+03 
c  Velocity[X]                                      0.27192E+02 
c  Velocity[Y]                                      0.47301E+01 
c  Velocity[Z]                                      0.21172E+02 
c  Pressure     0.38796E-04      25   0.14669E-02   0.56542E-01 0.19192E+03 
c  k            0.21943E-03      13   0.12176E-03   0.19060E-02 0.70113E+03 
c  omega        0.27926E+07       1   0.55149E-06   0.30011E+09 0.36477E+01 
c  TempK        0.67073E+04       9   0.27637E-05   0.15651E+04 0.28487E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.0129e-007           0.011             2             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.687          22.823      -0.0051109      0.00069073
v  Velocity[Y]             -16.754          15.573        0.034114         0.04451
v  Velocity[Z]              -25.98          12.128         -1.6559        -0.50274
v  ǁVelocityǁ         0.00015055          26.158           5.987          4.8674
v  Pressure                -612.61           159.8         -6.1319          8.8455
v  k                   2.1606e-014          8.1735       0.0046608        0.006277
v  omega                    3.9583     2.7317e+008     1.2898e+006           75374
v  TempK                    298.14          363.17          306.19          311.91
v  TurbVisc            1.7709e-022      0.00018899      2.362e-006     9.6851e-006
v  CourantNb           2.9707e-005           1.248         0.76033         0.97127
v  FourierNb             0.0031239               1         0.38111        0.077805
v  total_pressure      1.0071e+005     1.0148e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006            0.01      0.00010999      0.00030081

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.35          305.45
v  Yplus               0          2.9748          0.5344         0.35219


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.27646               2          1.1414          1.0491


 INSTANT    0.870000000E-03   TIME STEP NUMBER              87
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924678E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14451E-01 0.47301E+01
   Friction velocity        uk    :  0.14451E-01 0.47267E+01
   Dimensionless distance   yplus :  0.10369E-01 0.29736E+01
   Friction thermal sca.    tstar : -0.67365E-04 0.37414E+02
   Rough dim-less th. sca.  tplus :  0.73458E-02 0.21065E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         59 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17826E+00      11   0.54477E-05   0.52820E+02 0.21865E+03 
c  Velocity[X]                                      0.26997E+02 
c  Velocity[Y]                                      0.47095E+01 
c  Velocity[Z]                                      0.21114E+02 
c  Pressure     0.38606E-04      25   0.14679E-02   0.55892E-01 0.18750E+03 
c  k            0.22382E-03      13   0.13277E-03   0.18591E-02 0.67413E+03 
c  omega        0.27926E+07       1   0.54834E-06   0.29544E+09 0.35929E+01 
c  TempK        0.67194E+04       9   0.27009E-05   0.15363E+04 0.27757E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.9889e-007        0.010831             2             3


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.555          22.716       -0.005097      0.00055008
v  Velocity[Y]             -16.663          15.564        0.034573          0.0451
v  Velocity[Z]             -25.959          12.037         -1.6566        -0.50245
v  ǁVelocityǁ         0.00015103          26.137          6.0041          4.8784
v  Pressure                -608.18          160.98         -5.0822          9.8537
v  k                   3.9777e-014          8.2425       0.0047994       0.0063528
v  omega                    4.0341     2.7317e+008     1.2899e+006           75385
v  TempK                    298.14          363.17          306.35          311.95
v  TurbVisc            5.4439e-022      0.00019196     2.3888e-006       9.73e-006
v  CourantNb            3.571e-005          1.2517         0.76058         0.97132
v  FourierNb             0.0031986               1         0.38103        0.077645
v  total_pressure      1.0072e+005     1.0149e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006            0.01       0.0001095      0.00029946

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.35          305.45
v  Yplus               0          2.9736         0.53523         0.35385


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.25285               2          1.1416           1.049


 INSTANT    0.880000000E-03   TIME STEP NUMBER              88
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924736E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14480E-01 0.47302E+01
   Friction velocity        uk    :  0.14479E-01 0.47267E+01
   Dimensionless distance   yplus :  0.10390E-01 0.29724E+01
   Friction thermal sca.    tstar : -0.77420E-04 0.40927E+02
   Rough dim-less th. sca.  tplus :  0.73602E-02 0.21057E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         55 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17865E+00      11   0.54262E-05   0.52534E+02 0.21675E+03 
c  Velocity[X]                                      0.26794E+02 
c  Velocity[Y]                                      0.46850E+01 
c  Velocity[Z]                                      0.21055E+02 
c  Pressure     0.38617E-04      26   0.14494E-02   0.55555E-01 0.17956E+03 
c  k            0.22811E-03      13   0.15666E-03   0.18278E-02 0.64829E+03 
c  omega        0.27926E+07       1   0.54556E-06   0.29337E+09 0.35439E+01 
c  TempK        0.67315E+04       9   0.26380E-05   0.15086E+04 0.27031E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.9658e-007           0.011             2             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.464          22.592      -0.0050816      0.00041054
v  Velocity[Y]             -16.653          15.462        0.035027        0.045683
v  Velocity[Z]             -25.938          12.002         -1.6572        -0.50215
v  ǁVelocityǁ         0.00022103          26.117          6.0209          4.8892
v  Pressure                -603.45          162.11         -4.0803          10.813
v  k                   6.0621e-014          8.3023       0.0049389       0.0064289
v  omega                    4.1123     2.7317e+008     1.2899e+006           75396
v  TempK                    298.14          363.17          306.51          311.99
v  TurbVisc            1.0022e-021      0.00019418     2.4155e-006     9.7738e-006
v  CourantNb           3.5248e-005          1.2554         0.76083         0.97138
v  FourierNb             0.0032381               1         0.38094        0.077486
v  total_pressure      1.0072e+005     1.0149e+005     1.0132e+005     1.0134e+005
v  Local Time Step          1e-006            0.01      0.00010902      0.00029815

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.35          305.45
v  Yplus               0          2.9724         0.53603         0.35547


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.22464               2          1.1418          1.0489


 INSTANT    0.890000000E-03   TIME STEP NUMBER              89
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924700E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17914E-01 0.47302E+01
   Friction velocity        uk    :  0.17914E-01 0.47267E+01
   Dimensionless distance   yplus :  0.12854E-01 0.29713E+01
   Friction thermal sca.    tstar : -0.87496E-04 0.44683E+02
   Rough dim-less th. sca.  tplus :  0.91061E-02 0.21049E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         54 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17904E+00      11   0.54070E-05   0.52242E+02 0.21487E+03 
c  Velocity[X]                                      0.26590E+02 
c  Velocity[Y]                                      0.46586E+01 
c  Velocity[Z]                                      0.20993E+02 
c  Pressure     0.38581E-04      25   0.14187E-02   0.55165E-01 0.17403E+03 
c  k            0.23232E-03      13   0.17540E-03   0.18036E-02 0.62437E+03 
c  omega        0.27926E+07       1   0.54180E-06   0.28034E+09 0.34600E+01 
c  TempK        0.67436E+04       9   0.25759E-05   0.14820E+04 0.26320E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      7.945e-007           0.011             2             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.371          22.453      -0.0050643      0.00027343
v  Velocity[Y]             -17.045          15.391        0.035477         0.04625
v  Velocity[Z]             -25.918          12.034         -1.6577        -0.50184
v  ǁVelocityǁ         0.00025932          26.098          6.0375          4.9001
v  Pressure                -597.77          163.21         -3.1118          11.738
v  k                   8.3403e-014          8.3659       0.0050797       0.0065054
v  omega                    4.1931     2.7316e+008     1.2899e+006           75406
v  TempK                    298.14          363.17          306.67          312.03
v  TurbVisc            1.5274e-021      0.00019603      2.442e-006     9.8171e-006
v  CourantNb           3.4582e-005          1.2586         0.76107         0.97144
v  FourierNb             0.0032279               1         0.38086        0.077329
v  total_pressure      1.0073e+005     1.0149e+005     1.0132e+005     1.0134e+005
v  Local Time Step          1e-006            0.01      0.00010856       0.0002969

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.35          305.45
v  Yplus               0          2.9713         0.53681         0.35706


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.3217               2          1.1419          1.0488


 INSTANT    0.900000000E-03   TIME STEP NUMBER              90
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924763E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14029E-01 0.47301E+01
   Friction velocity        uk    :  0.14029E-01 0.47265E+01
   Dimensionless distance   yplus :  0.10066E-01 0.29702E+01
   Friction thermal sca.    tstar : -0.97286E-04 0.48542E+02
   Rough dim-less th. sca.  tplus :  0.71311E-02 0.21041E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         59 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17943E+00      11   0.53970E-05   0.51973E+02 0.21304E+03 
c  Velocity[X]                                      0.26393E+02 
c  Velocity[Y]                                      0.46416E+01 
c  Velocity[Z]                                      0.20938E+02 
c  Pressure     0.38361E-04      25   0.13901E-02   0.54527E-01 0.16449E+03 
c  k            0.23649E-03      13   0.17146E-03   0.17813E-02 0.60348E+03 
c  omega        0.27926E+07       1   0.53839E-06   0.27432E+09 0.33946E+01 
c  TempK        0.67557E+04       8   0.49706E-05   0.14507E+04 0.25588E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.9205e-007           0.011             2             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.264          22.378       -0.005038       0.0001485
v  Velocity[Y]             -16.537          15.353        0.035926        0.046804
v  Velocity[Z]               -25.9           12.13         -1.6583        -0.50153
v  ǁVelocityǁ         0.00019161          26.081          6.0538          4.9109
v  Pressure                -592.83          164.25         -2.2047          12.601
v  k                   1.0729e-013            8.44       0.0052218       0.0065824
v  omega                    4.2766     2.7316e+008     1.2899e+006           75417
v  TempK                    298.14          363.17          306.82          312.07
v  TurbVisc            2.1014e-021      0.00019781     2.4684e-006       9.86e-006
v  CourantNb           3.4894e-005          1.2625         0.76131          0.9715
v  FourierNb             0.0032182               1         0.38078        0.077171
v  total_pressure      1.0073e+005     1.0149e+005     1.0132e+005     1.0134e+005
v  Local Time Step          1e-006            0.01       0.0001081      0.00029565

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.35          305.45
v  Yplus               0          2.9702         0.53755         0.35861


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.23679               2          1.1421          1.0487


 INSTANT    0.910000000E-03   TIME STEP NUMBER              91
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924721E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16320E-01 0.47300E+01
   Friction velocity        uk    :  0.16320E-01 0.47264E+01
   Dimensionless distance   yplus :  0.11711E-01 0.29692E+01
   Friction thermal sca.    tstar : -0.10656E-03 0.52191E+02
   Rough dim-less th. sca.  tplus :  0.82959E-02 0.21034E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.17982E+00      11   0.53835E-05   0.51698E+02 0.21122E+03 
c  Velocity[X]                                      0.26199E+02 
c  Velocity[Y]                                      0.46162E+01 
c  Velocity[Z]                                      0.20883E+02 
c  Pressure     0.38341E-04      24   0.13789E-02   0.54183E-01 0.16132E+03 
c  k            0.24059E-03      13   0.18496E-03   0.18040E-02 0.58610E+03 
c  omega        0.27926E+07       1   0.53531E-06   0.27420E+09 0.33463E+01 
c  TempK        0.67678E+04       8   0.48528E-05   0.14264E+04 0.24945E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8948e-007           0.011             2             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.143          22.298      -0.0050074     3.4402e-005
v  Velocity[Y]             -16.421          15.443        0.036386        0.047352
v  Velocity[Z]             -25.881          12.282         -1.6588        -0.50122
v  ǁVelocityǁ         0.00019164          26.063          6.0699          4.9216
v  Pressure                -588.58          165.26         -1.3171          13.441
v  k                   1.3161e-013           8.527       0.0053654       0.0066602
v  omega                     4.363     2.7316e+008     1.2899e+006           75427
v  TempK                    298.14          363.17          306.97          312.12
v  TurbVisc            2.7032e-021      0.00019972     2.4945e-006      9.902e-006
v  CourantNb           3.5021e-005          1.2666         0.76155         0.97156
v  FourierNb             0.0032089               1         0.38071        0.077015
v  total_pressure      1.0074e+005     1.0149e+005     1.0132e+005     1.0134e+005
v  Local Time Step          1e-006            0.01      0.00010764      0.00029441

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.35          305.46
v  Yplus               0          2.9692         0.53828         0.36013


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.20874               2          1.1423          1.0486


 INSTANT    0.920000000E-03   TIME STEP NUMBER              92
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924714E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16329E-01 0.47299E+01
   Friction velocity        uk    :  0.16329E-01 0.47262E+01
   Dimensionless distance   yplus :  0.11717E-01 0.29681E+01
   Friction thermal sca.    tstar : -0.11520E-03 0.55233E+02
   Rough dim-less th. sca.  tplus :  0.83004E-02 0.21026E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18022E+00      11   0.53759E-05   0.51437E+02 0.20946E+03 
c  Velocity[X]                                      0.26011E+02 
c  Velocity[Y]                                      0.46018E+01 
c  Velocity[Z]                                      0.20824E+02 
c  Pressure     0.38178E-04      25   0.13439E-02   0.53647E-01 0.15753E+03 
c  k            0.24461E-03      13   0.15550E-03   0.17811E-02 0.56995E+03 
c  omega        0.27926E+07       1   0.53168E-06   0.26629E+09 0.32743E+01 
c  TempK        0.67798E+04       8   0.47396E-05   0.14031E+04 0.24347E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8733e-007           0.011             2             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.011          22.203       -0.004967    -8.0531e-005
v  Velocity[Y]             -16.349          15.333        0.036838        0.047889
v  Velocity[Z]             -25.863          12.535         -1.6593         -0.5009
v  ǁVelocityǁ         0.00018485          26.046          6.0857          4.9323
v  Pressure                -586.91          166.26        -0.44976           14.26
v  k                   1.5561e-013          8.6268       0.0055107       0.0067389
v  omega                    4.4523     2.7316e+008     1.2899e+006           75438
v  TempK                    298.14          363.17          307.13          312.16
v  TurbVisc             3.316e-021      0.00020186     2.5206e-006     9.9447e-006
v  CourantNb           3.5504e-005          1.2701         0.76178         0.97161
v  FourierNb             0.0031973               1         0.38064        0.076868
v  total_pressure      1.0074e+005     1.0149e+005     1.0132e+005     1.0134e+005
v  Local Time Step          1e-006            0.01       0.0001072      0.00029322

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.35          305.46
v  Yplus               0          2.9681         0.53897         0.36162


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.37553               2          1.1424          1.0485


 INSTANT    0.930000000E-03   TIME STEP NUMBER              93
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924687E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15677E-01 0.47298E+01
   Friction velocity        uk    :  0.15677E-01 0.47260E+01
   Dimensionless distance   yplus :  0.11249E-01 0.29671E+01
   Friction thermal sca.    tstar : -0.12302E-03 0.57147E+02
   Rough dim-less th. sca.  tplus :  0.79691E-02 0.21019E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18061E+00      11   0.53661E-05   0.51168E+02 0.20769E+03 
c  Velocity[X]                                      0.25814E+02 
c  Velocity[Y]                                      0.45814E+01 
c  Velocity[Z]                                      0.20773E+02 
c  Pressure     0.38201E-04      24   0.13329E-02   0.53380E-01 0.15254E+03 
c  k            0.24853E-03      13   0.11855E-03   0.17882E-02 0.55780E+03 
c  omega        0.27926E+07       1   0.52855E-06   0.26258E+09 0.32139E+01 
c  TempK        0.67918E+04       8   0.46330E-05   0.13807E+04 0.23803E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8544e-007           0.011             2             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -21.867          22.117      -0.0049271     -0.00021127
v  Velocity[Y]             -16.504          15.217         0.03729        0.048426
v  Velocity[Z]             -25.846          12.893         -1.6598        -0.50058
v  ǁVelocityǁ         0.00029251          26.029          6.1013           4.943
v  Pressure                -585.38          167.24         0.38922          15.049
v  k                   1.5965e-013          8.7344       0.0056579       0.0068188
v  omega                    4.5445     2.7316e+008     1.2899e+006           75449
v  TempK                    298.14          363.17          307.28           312.2
v  TurbVisc            3.9207e-021      0.00020427      2.547e-006     9.9888e-006
v  CourantNb           3.7586e-005          1.2732         0.76201         0.97166
v  FourierNb             0.0031878               1         0.38057        0.076731
v  total_pressure      1.0074e+005     1.0149e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006            0.01      0.00010677       0.0002921

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.35          305.46
v  Yplus               0          2.9671         0.53965         0.36309


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.29469               2          1.1426          1.0484


 INSTANT    0.940000000E-03   TIME STEP NUMBER              94
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924712E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.20189E-01 0.47296E+01
   Friction velocity        uk    :  0.20189E-01 0.47258E+01
   Dimensionless distance   yplus :  0.14487E-01 0.29662E+01
   Friction thermal sca.    tstar : -0.12974E-03 0.57712E+02
   Rough dim-less th. sca.  tplus :  0.10262E-01 0.21013E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18101E+00      11   0.53522E-05   0.50905E+02 0.20596E+03 
c  Velocity[X]                                      0.25619E+02 
c  Velocity[Y]                                      0.45716E+01 
c  Velocity[Z]                                      0.20715E+02 
c  Pressure     0.38227E-04      25   0.12971E-02   0.53124E-01 0.14788E+03 
c  k            0.25233E-03      13   0.78390E-04   0.18612E-02 0.55139E+03 
c  omega        0.27926E+07       1   0.52376E-06   0.24224E+09 0.30933E+01 
c  TempK        0.68038E+04       8   0.45353E-05   0.13591E+04 0.23318E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8384e-007           0.011             2             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -21.714          22.026      -0.0048804      -0.0003415
v  Velocity[Y]             -16.208          15.143        0.037749        0.048969
v  Velocity[Z]              -25.83          13.398         -1.6602        -0.50024
v  ǁVelocityǁ         0.00038376          26.014          6.1167          4.9536
v  Pressure                -583.82          168.19           1.202          15.813
v  k                   1.6058e-013          8.8465        0.005807          0.0069
v  omega                    4.6397     2.7316e+008     1.2899e+006           75459
v  TempK                    298.14          363.17          307.43          312.24
v  TurbVisc            4.0415e-021      0.00020684     2.5734e-006     1.0034e-005
v  CourantNb           4.0773e-005          1.2758         0.76224         0.97171
v  FourierNb             0.0031806               1         0.38051        0.076601
v  total_pressure      1.0074e+005     1.0149e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006            0.01      0.00010635      0.00029101

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.36          305.46
v  Yplus               0          2.9662         0.54032         0.36453


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41706               2          1.1428          1.0483


 INSTANT    0.950000000E-03   TIME STEP NUMBER              95
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924700E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.23126E-01 0.47294E+01
   Friction velocity        uk    :  0.23126E-01 0.47256E+01
   Dimensionless distance   yplus :  0.16594E-01 0.29652E+01
   Friction thermal sca.    tstar : -0.13543E-03 0.57134E+02
   Rough dim-less th. sca.  tplus :  0.11755E-01 0.21006E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18142E+00      11   0.53507E-05   0.50639E+02 0.20426E+03 
c  Velocity[X]                                      0.25432E+02 
c  Velocity[Y]                                      0.45533E+01 
c  Velocity[Z]                                      0.20653E+02 
c  Pressure     0.38437E-04      26   0.13042E-02   0.53122E-01 0.14502E+03 
c  k            0.25598E-03      13   0.10054E-03   0.19746E-02 0.55062E+03 
c  omega        0.27925E+07       1   0.52113E-06   0.24284E+09 0.30477E+01 
c  TempK        0.68158E+04       8   0.44480E-05   0.13383E+04 0.22897E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8248e-007           0.011             2             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -21.564          21.923      -0.0048347     -0.00047587
v  Velocity[Y]             -16.105          15.207        0.038212        0.049522
v  Velocity[Z]             -25.814          14.039         -1.6607         -0.4999
v  ǁVelocityǁ         0.00040569          25.999          6.1319          4.9642
v  Pressure                -582.04          169.12          1.9986           16.56
v  k                   1.6176e-013          8.9631       0.0059583       0.0069829
v  omega                    4.7378     2.7316e+008     1.2899e+006           75470
v  TempK                    298.14          363.17          307.58          312.28
v  TurbVisc             4.065e-021      0.00020953        2.6e-006     1.0079e-005
v  CourantNb           4.2581e-005           1.278         0.76246         0.97176
v  FourierNb             0.0031756               1         0.38046        0.076485
v  total_pressure      1.0074e+005     1.0149e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006            0.01      0.00010594      0.00028997

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.36          305.46
v  Yplus               0          2.9652         0.54097         0.36593


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47061               2          1.1429          1.0482


 INSTANT    0.960000000E-03   TIME STEP NUMBER              96
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924735E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.19887E-01 0.47291E+01
   Friction velocity        uk    :  0.19887E-01 0.47252E+01
   Dimensionless distance   yplus :  0.13625E-01 0.29643E+01
   Friction thermal sca.    tstar : -0.14022E-03 0.56185E+02
   Rough dim-less th. sca.  tplus :  0.96521E-02 0.20999E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18182E+00      11   0.53600E-05   0.50356E+02 0.20257E+03 
c  Velocity[X]                                      0.25241E+02 
c  Velocity[Y]                                      0.45399E+01 
c  Velocity[Z]                                      0.20576E+02 
c  Pressure     0.38343E-04      24   0.12935E-02   0.52699E-01 0.14022E+03 
c  k            0.25950E-03      13   0.15499E-03   0.20775E-02 0.55078E+03 
c  omega        0.27925E+07       1   0.51891E-06   0.23711E+09 0.30038E+01 
c  TempK        0.68278E+04       8   0.43727E-05   0.13184E+04 0.22542E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8145e-007        0.010829             3             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -21.465          21.809      -0.0047839     -0.00060411
v  Velocity[Y]              -16.08          15.083        0.038668        0.050072
v  Velocity[Z]             -25.799          14.861         -1.6611        -0.49956
v  ǁVelocityǁ         0.00039354          25.984          6.1468          4.9748
v  Pressure                 -580.3          170.03          2.7665          17.278
v  k                   1.6321e-013           9.083       0.0061119       0.0070676
v  omega                    4.8389     2.7316e+008     1.2899e+006           75480
v  TempK                    298.14          363.17          307.74          312.32
v  TurbVisc            4.0949e-021      0.00021237     2.6268e-006     1.0126e-005
v  CourantNb           4.1605e-005          1.2797         0.76269         0.97181
v  FourierNb             0.0031697               1         0.38042        0.076381
v  total_pressure      1.0074e+005      1.015e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006            0.01      0.00010554      0.00028896

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.36          305.46
v  Yplus               0          2.9643          0.5416         0.36731


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54379               2          1.1431          1.0482


 INSTANT    0.970000000E-03   TIME STEP NUMBER              97
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924642E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.20804E-01 0.47287E+01
   Friction velocity        uk    :  0.20804E-01 0.47248E+01
   Dimensionless distance   yplus :  0.14254E-01 0.29633E+01
   Friction thermal sca.    tstar : -0.14431E-03 0.55033E+02
   Rough dim-less th. sca.  tplus :  0.10097E-01 0.20992E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18222E+00      11   0.53521E-05   0.50076E+02 0.20092E+03 
c  Velocity[X]                                      0.25058E+02 
c  Velocity[Y]                                      0.45209E+01 
c  Velocity[Z]                                      0.20497E+02 
c  Pressure     0.38059E-04      25   0.12717E-02   0.52014E-01 0.13426E+03 
c  k            0.26292E-03      13   0.20197E-03   0.21590E-02 0.54879E+03 
c  omega        0.27925E+07       1   0.51649E-06   0.23497E+09 0.29551E+01 
c  TempK        0.68397E+04       8   0.43104E-05   0.12992E+04 0.22252E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8064e-007        0.010553             3             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -21.356          21.685      -0.0047318     -0.00072033
v  Velocity[Y]             -16.908          14.949        0.039118        0.050612
v  Velocity[Z]             -25.785           15.96         -1.6615        -0.49921
v  ǁVelocityǁ         0.00035422           25.97          6.1616          4.9853
v  Pressure                -578.66          170.89          3.4912          17.951
v  k                   1.6495e-013          9.2045        0.006268       0.0071546
v  omega                    4.9431     2.7316e+008     1.2899e+006           75490
v  TempK                    298.13          363.17          307.89          312.37
v  TurbVisc            4.1315e-021      0.00021532     2.6538e-006     1.0174e-005
v  CourantNb           4.4135e-005           1.281         0.76291         0.97186
v  FourierNb             0.0031626               1         0.38037        0.076289
v  total_pressure      1.0075e+005      1.015e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006            0.01      0.00010515      0.00028797

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.36          305.46
v  Yplus               0          2.9633         0.54221         0.36867


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43823               2          1.1433          1.0481


 INSTANT    0.980000000E-03   TIME STEP NUMBER              98
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924704E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18816E-01 0.47282E+01
   Friction velocity        uk    :  0.18816E-01 0.47243E+01
   Dimensionless distance   yplus :  0.12892E-01 0.29625E+01
   Friction thermal sca.    tstar : -0.15253E-03 0.52285E+02
   Rough dim-less th. sca.  tplus :  0.91325E-02 0.20986E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18263E+00      11   0.53450E-05   0.49804E+02 0.19934E+03 
c  Velocity[X]                                      0.24877E+02 
c  Velocity[Y]                                      0.45127E+01 
c  Velocity[Z]                                      0.20414E+02 
c  Pressure     0.37816E-04      24   0.12543E-02   0.51400E-01 0.12869E+03 
c  k            0.26622E-03      13   0.20913E-03   0.21999E-02 0.54523E+03 
c  omega        0.27925E+07       1   0.51350E-06   0.22450E+09 0.28806E+01 
c  TempK        0.68516E+04       8   0.42615E-05   0.12807E+04 0.22028E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8005e-007         0.01017             3             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -21.237          21.552       -0.004673     -0.00083663
v  Velocity[Y]             -16.052          14.865        0.039574        0.051148
v  Velocity[Z]             -25.771          17.457         -1.6619        -0.49887
v  ǁVelocityǁ         0.00039352          25.957          6.1761          4.9958
v  Pressure                -576.96          171.71           4.178          18.585
v  k                   1.6706e-013          9.3269       0.0064267       0.0072442
v  omega                    5.0507     2.7317e+008     1.2899e+006           75501
v  TempK                    298.13          363.17          308.04          312.41
v  TurbVisc            4.1757e-021      0.00021835     2.6812e-006     1.0225e-005
v  CourantNb           3.9317e-005           1.282         0.76312         0.97189
v  FourierNb             0.0031556               1         0.38034        0.076212
v  total_pressure      1.0075e+005      1.015e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006            0.01      0.00010476      0.00028701

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.36          305.46
v  Yplus               0          2.9625         0.54281         0.36998


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.27621               2          1.1435          1.0481


 INSTANT    0.990000000E-03   TIME STEP NUMBER              99
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924752E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16012E-01 0.47275E+01
   Friction velocity        uk    :  0.16011E-01 0.47236E+01
   Dimensionless distance   yplus :  0.10970E-01 0.29616E+01
   Friction thermal sca.    tstar : -0.16343E-03 0.50513E+02
   Rough dim-less th. sca.  tplus :  0.77711E-02 0.20980E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18304E+00      11   0.53245E-05   0.49526E+02 0.19777E+03 
c  Velocity[X]                                      0.24692E+02 
c  Velocity[Y]                                      0.44908E+01 
c  Velocity[Z]                                      0.20343E+02 
c  Pressure     0.37849E-04      24   0.12432E-02   0.51172E-01 0.12433E+03 
c  k            0.26945E-03      13   0.19939E-03   0.22064E-02 0.54011E+03 
c  omega        0.27925E+07       1   0.51057E-06   0.21337E+09 0.28002E+01 
c  TempK        0.68635E+04       8   0.42260E-05   0.12629E+04 0.21865E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.7966e-007                             3


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -21.109          21.411      -0.0046184      -0.0009698
v  Velocity[Y]             -16.001          14.854        0.040022        0.051685
v  Velocity[Z]             -25.758          19.318         -1.6622        -0.49851
v  ǁVelocityǁ         0.00043457          25.945          6.1905          5.0062
v  Pressure                -575.06          172.51          4.8399          19.194
v  k                   1.6959e-013          9.4492        0.006588       0.0073367
v  omega                    5.1615     2.7317e+008     1.2899e+006           75511
v  TempK                    298.13          363.17           308.2          312.45
v  TurbVisc             4.229e-021      0.00022144     2.7088e-006     1.0279e-005
v  CourantNb           4.2128e-005          1.2826         0.76333         0.97193
v  FourierNb             0.0031487               1         0.38031        0.076151
v  total_pressure      1.0075e+005      1.015e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0097823      0.00010439      0.00028609

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.36          305.46
v  Yplus               0          2.9616         0.54338         0.37127


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.23493               2          1.1436          1.0481


 INSTANT    0.100000000E-02   TIME STEP NUMBER             100
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924734E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.24595E-01 0.47267E+01
   Friction velocity        uk    :  0.24595E-01 0.47228E+01
   Dimensionless distance   yplus :  0.17648E-01 0.29608E+01
   Friction thermal sca.    tstar : -0.17255E-03 0.52466E+02
   Rough dim-less th. sca.  tplus :  0.12502E-01 0.20974E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18344E+00      11   0.53125E-05   0.49236E+02 0.19623E+03 
c  Velocity[X]                                      0.24517E+02 
c  Velocity[Y]                                      0.44769E+01 
c  Velocity[Z]                                      0.20242E+02 
c  Pressure     0.37770E-04      24   0.12602E-02   0.50810E-01 0.12218E+03 
c  k            0.27263E-03      13   0.17749E-03   0.21871E-02 0.53449E+03 
c  omega        0.27925E+07       1   0.50893E-06   0.21445E+09 0.27739E+01 
c  TempK        0.68754E+04       8   0.42034E-05   0.12457E+04 0.21760E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      7.795e-007                             3


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -20.973          21.265      -0.0045636      -0.0010981
v  Velocity[Y]             -16.024          14.858        0.040468        0.052224
v  Velocity[Z]             -25.746          20.342         -1.6626        -0.49815
v  ǁVelocityǁ         0.00048557          25.933          6.2047          5.0166
v  Pressure                -572.99          173.29          5.4901          19.792
v  k                   1.7269e-013          9.5704        0.006752       0.0074327
v  omega                    5.2755     2.7317e+008       1.29e+006           75522
v  TempK                    298.13          363.17          308.35          312.49
v  TurbVisc            4.2931e-021      0.00022457     2.7367e-006     1.0335e-005
v  CourantNb           4.6974e-005          1.2829         0.76353         0.97197
v  FourierNb              0.003142               1         0.38028        0.076107
v  total_pressure      1.0075e+005      1.015e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0093292      0.00010403      0.00028519

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.36          305.46
v  Yplus               0          2.9608         0.54394         0.37254


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.3867               2          1.1438          1.0481


 INSTANT    0.101000000E-02   TIME STEP NUMBER             101
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924739E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.25936E-01 0.47257E+01
   Friction velocity        uk    :  0.25936E-01 0.47218E+01
   Dimensionless distance   yplus :  0.18593E-01 0.29599E+01
   Friction thermal sca.    tstar : -0.17949E-03 0.54506E+02
   Rough dim-less th. sca.  tplus :  0.13172E-01 0.20968E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18385E+00      11   0.53093E-05   0.48967E+02 0.19473E+03 
c  Velocity[X]                                      0.24342E+02 
c  Velocity[Y]                                      0.44661E+01 
c  Velocity[Z]                                      0.20159E+02 
c  Pressure     0.37771E-04      25   0.12275E-02   0.50574E-01 0.11796E+03 
c  k            0.27577E-03      13   0.15276E-03   0.21443E-02 0.52799E+03 
c  omega        0.27925E+07       1   0.50818E-06   0.21982E+09 0.27728E+01 
c  TempK        0.68872E+04       8   0.41929E-05   0.12291E+04 0.21707E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.7959e-007                             3


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -20.831          21.114      -0.0045085      -0.0012185
v  Velocity[Y]             -17.029          14.789        0.040899        0.052765
v  Velocity[Z]             -25.734          20.672          -1.663         -0.4978
v  ǁVelocityǁ         0.00051657          25.921          6.2186          5.0269
v  Pressure                -570.38          174.04          6.1095          20.357
v  k                   1.7649e-013          9.6803       0.0069188       0.0075324
v  omega                    5.3927     2.7318e+008       1.29e+006           75532
v  TempK                    298.13          363.17          308.51          312.53
v  TurbVisc            4.3715e-021      0.00022772     2.7651e-006     1.0397e-005
v  CourantNb           4.6703e-005          1.2827         0.76374         0.97202
v  FourierNb             0.0031354               1         0.38026        0.076082
v  total_pressure      1.0075e+005      1.015e+005     1.0133e+005     1.0135e+005
v  Local Time Step          1e-006       0.0088353      0.00010368      0.00028433

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.36          305.46
v  Yplus               0          2.9599         0.54448         0.37378


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40007               2           1.144          1.0481


 INSTANT    0.102000000E-02   TIME STEP NUMBER             102
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924789E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.22489E-01 0.47246E+01
   Friction velocity        uk    :  0.22489E-01 0.47207E+01
   Dimensionless distance   yplus :  0.16123E-01 0.29590E+01
   Friction thermal sca.    tstar : -0.18411E-03 0.56548E+02
   Rough dim-less th. sca.  tplus :  0.11421E-01 0.20962E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18426E+00      11   0.53180E-05   0.48717E+02 0.19328E+03 
c  Velocity[X]                                      0.24174E+02 
c  Velocity[Y]                                      0.44581E+01 
c  Velocity[Z]                                      0.20085E+02 
c  Pressure     0.37664E-04      24   0.12151E-02   0.50208E-01 0.11429E+03 
c  k            0.27888E-03      13   0.13024E-03   0.21136E-02 0.52276E+03 
c  omega        0.27925E+07       1   0.50633E-06   0.21756E+09 0.27440E+01 
c  TempK        0.68990E+04       8   0.41931E-05   0.12130E+04 0.21699E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      7.799e-007                             3


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -20.684           20.96      -0.0044458      -0.0013367
v  Velocity[Y]             -16.093          14.681        0.041331        0.053307
v  Velocity[Z]             -25.722          21.143         -1.6634        -0.49748
v  ǁVelocityǁ         0.00056016           25.91          6.2324          5.0372
v  Pressure                 -567.6          174.76          6.7062          20.901
v  k                   1.8102e-013          9.7582       0.0070882       0.0076362
v  omega                    5.5131     2.7318e+008       1.29e+006           75542
v  TempK                    298.13          363.17          308.67          312.58
v  TurbVisc            4.4677e-021      0.00023068     2.7942e-006     1.0463e-005
v  CourantNb           4.5656e-005          1.2822         0.76394         0.97206
v  FourierNb             0.0031289               1         0.38025        0.076078
v  total_pressure      1.0076e+005      1.015e+005     1.0133e+005     1.0135e+005
v  Local Time Step          1e-006       0.0083523      0.00010334       0.0002835

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.37          305.46
v  Yplus               0           2.959         0.54501         0.37499


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.27416               2          1.1442          1.0481


 INSTANT    0.103000000E-02   TIME STEP NUMBER             103
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924846E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.24893E-01 0.47234E+01
   Friction velocity        uk    :  0.24893E-01 0.47194E+01
   Dimensionless distance   yplus :  0.17846E-01 0.29582E+01
   Friction thermal sca.    tstar : -0.18647E-03 0.58583E+02
   Rough dim-less th. sca.  tplus :  0.12642E-01 0.20956E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18467E+00      11   0.53097E-05   0.48453E+02 0.19185E+03 
c  Velocity[X]                                      0.24002E+02 
c  Velocity[Y]                                      0.44356E+01 
c  Velocity[Z]                                      0.20015E+02 
c  Pressure     0.37698E-04      25   0.11800E-02   0.50044E-01 0.11229E+03 
c  k            0.28197E-03      13   0.11338E-03   0.21136E-02 0.51892E+03 
c  omega        0.27925E+07       1   0.50336E-06   0.19754E+09 0.26377E+01 
c  TempK        0.69107E+04       8   0.42022E-05   0.11973E+04 0.21730E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      7.804e-007                             3


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -20.544          20.803      -0.0043818      -0.0014649
v  Velocity[Y]             -16.062          14.608        0.041756        0.053853
v  Velocity[Z]             -25.711          22.013         -1.6637        -0.49717
v  ǁVelocityǁ          0.0006023          25.899          6.2461          5.0474
v  Pressure                -564.65          175.47          7.2896          21.427
v  k                   1.8628e-013          9.7972       0.0072605       0.0077447
v  omega                    5.6368     2.7318e+008       1.29e+006           75552
v  TempK                    298.13          363.17          308.83          312.62
v  TurbVisc            4.5824e-021      0.00023307     2.8241e-006     1.0534e-005
v  CourantNb           4.4801e-005          1.2814         0.76414         0.97209
v  FourierNb             0.0031224               1         0.38024        0.076092
v  total_pressure      1.0076e+005      1.015e+005     1.0133e+005     1.0135e+005
v  Local Time Step          1e-006       0.0078141      0.00010302      0.00028268

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.37          305.46
v  Yplus               0          2.9582         0.54554         0.37619


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.18132               2          1.1444          1.0482


 INSTANT    0.104000000E-02   TIME STEP NUMBER             104
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924819E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.26330E-01 0.47221E+01
   Friction velocity        uk    :  0.26330E-01 0.47181E+01
   Dimensionless distance   yplus :  0.18876E-01 0.29573E+01
   Friction thermal sca.    tstar : -0.19412E-03 0.60572E+02
   Rough dim-less th. sca.  tplus :  0.13372E-01 0.20950E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18507E+00      11   0.53033E-05   0.48193E+02 0.19046E+03 
c  Velocity[X]                                      0.23836E+02 
c  Velocity[Y]                                      0.44233E+01 
c  Velocity[Z]                                      0.19933E+02 
c  Pressure     0.37540E-04      25   0.11643E-02   0.49634E-01 0.10990E+03 
c  k            0.28506E-03      13   0.10239E-03   0.21507E-02 0.51611E+03 
c  omega        0.27925E+07       1   0.50165E-06   0.19334E+09 0.26014E+01 
c  TempK        0.69225E+04       8   0.42187E-05   0.11819E+04 0.21792E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8109e-007                             3


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -20.448          20.647      -0.0043092      -0.0015925
v  Velocity[Y]             -16.066          14.567        0.042177        0.054393
v  Velocity[Z]             -25.701          20.887          -1.664        -0.49687
v  ǁVelocityǁ         0.00067374          25.889          6.2595          5.0576
v  Pressure                -561.36          176.16          7.8607          21.942
v  k                    1.923e-013          9.7841       0.0074356       0.0078583
v  omega                    5.7639     2.7319e+008       1.29e+006           75562
v  TempK                    298.13          363.17          308.99          312.66
v  TurbVisc            4.7154e-021      0.00023499     2.8546e-006      1.061e-005
v  CourantNb           4.3955e-005          1.2803         0.76433         0.97212
v  FourierNb             0.0031159               1         0.38024        0.076124
v  total_pressure      1.0076e+005      1.015e+005     1.0133e+005     1.0135e+005
v  Local Time Step          1e-006        0.007299       0.0001027      0.00028187

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.37          305.46
v  Yplus               0          2.9573         0.54606         0.37736


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38295               2          1.1446          1.0482


 INSTANT    0.105000000E-02   TIME STEP NUMBER             105
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924666E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.27788E-01 0.47208E+01
   Friction velocity        uk    :  0.27788E-01 0.47168E+01
   Dimensionless distance   yplus :  0.19921E-01 0.29565E+01
   Friction thermal sca.    tstar : -0.20372E-03 0.62500E+02
   Rough dim-less th. sca.  tplus :  0.14112E-01 0.20944E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18548E+00      11   0.53019E-05   0.47927E+02 0.18908E+03 
c  Velocity[X]                                      0.23667E+02 
c  Velocity[Y]                                      0.44079E+01 
c  Velocity[Z]                                      0.19852E+02 
c  Pressure     0.37427E-04      25   0.11328E-02   0.49294E-01 0.11125E+03 
c  k            0.28816E-03      13   0.99904E-04   0.22310E-02 0.51453E+03 
c  omega        0.27925E+07       1   0.50108E-06   0.20568E+09 0.26237E+01 
c  TempK        0.69342E+04       8   0.42408E-05   0.11669E+04 0.21880E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8194e-007                             3


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -20.344          20.491       -0.004233      -0.0017275
v  Velocity[Y]             -16.348          15.393        0.042591        0.054925
v  Velocity[Z]             -25.691          18.146         -1.6644        -0.49657
v  ǁVelocityǁ         0.00065671          25.879          6.2728          5.0678
v  Pressure                -557.96          176.88          8.4482          22.473
v  k                   1.9917e-013          9.7158       0.0076139       0.0079776
v  omega                     5.894     2.7319e+008       1.29e+006           75573
v  TempK                    298.13          363.17          309.15           312.7
v  TurbVisc             4.868e-021      0.00023602     2.8858e-006     1.0693e-005
v  CourantNb            4.261e-005          1.2789         0.76453         0.97216
v  FourierNb             0.0031095               1         0.38024        0.076171
v  total_pressure      1.0077e+005      1.015e+005     1.0133e+005     1.0135e+005
v  Local Time Step          1e-006       0.0075446      0.00010239      0.00028106

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.37          305.46
v  Yplus               0          2.9565         0.54657          0.3785


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.26701               2          1.1448          1.0483


 INSTANT    0.106000000E-02   TIME STEP NUMBER             106
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924877E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.27656E-01 0.47193E+01
   Friction velocity        uk    :  0.27656E-01 0.47153E+01
   Dimensionless distance   yplus :  0.19827E-01 0.29556E+01
   Friction thermal sca.    tstar : -0.21303E-03 0.64154E+02
   Rough dim-less th. sca.  tplus :  0.14045E-01 0.20938E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18589E+00      11   0.53152E-05   0.47677E+02 0.18774E+03 
c  Velocity[X]                                      0.23506E+02 
c  Velocity[Y]                                      0.44003E+01 
c  Velocity[Z]                                      0.19771E+02 
c  Pressure     0.37432E-04      25   0.11173E-02   0.49120E-01 0.10825E+03 
c  k            0.29128E-03      13   0.10834E-03   0.23708E-02 0.51427E+03 
c  omega        0.27925E+07       1   0.49913E-06   0.19829E+09 0.25738E+01 
c  TempK        0.69459E+04       8   0.42662E-05   0.11521E+04 0.21986E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8304e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -20.234          20.378      -0.0041556      -0.0018581
v  Velocity[Y]             -16.195          14.573        0.042998        0.055454
v  Velocity[Z]             -25.682           15.15         -1.6647        -0.49627
v  ǁVelocityǁ         0.00072919           25.87           6.286          5.0779
v  Pressure                -554.36          177.58          9.0144          22.982
v  k                    1.337e-013          9.5961       0.0077956       0.0081028
v  omega                    6.0271     2.7319e+008       1.29e+006           75583
v  TempK                    298.13          363.17          309.31          312.74
v  TurbVisc             5.042e-021      0.00023595     2.9179e-006     1.0783e-005
v  CourantNb           4.1079e-005          1.2771         0.76472         0.97219
v  FourierNb             0.0031031               1         0.38025        0.076232
v  total_pressure      1.0077e+005      1.015e+005     1.0133e+005     1.0135e+005
v  Local Time Step          1e-006       0.0077523      0.00010209      0.00028025

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.37          305.46
v  Yplus               0          2.9556         0.54707         0.37963


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.21935               2           1.145          1.0484


 INSTANT    0.107000000E-02   TIME STEP NUMBER             107
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924754E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.27557E-01 0.47178E+01
   Friction velocity        uk    :  0.27557E-01 0.47138E+01
   Dimensionless distance   yplus :  0.19755E-01 0.29549E+01
   Friction thermal sca.    tstar : -0.22183E-03 0.65339E+02
   Rough dim-less th. sca.  tplus :  0.13995E-01 0.20932E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18630E+00      11   0.53276E-05   0.47410E+02 0.18637E+03 
c  Velocity[X]                                      0.23343E+02 
c  Velocity[Y]                                      0.43766E+01 
c  Velocity[Z]                                      0.19690E+02 
c  Pressure     0.37368E-04      26   0.11150E-02   0.48859E-01 0.10830E+03 
c  k            0.29445E-03      13   0.12656E-03   0.25637E-02 0.51552E+03 
c  omega        0.27925E+07       1   0.49645E-06   0.18340E+09 0.24859E+01 
c  TempK        0.69576E+04       8   0.42934E-05   0.11376E+04 0.22104E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8297e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -20.119          20.289      -0.0040762      -0.0019888
v  Velocity[Y]             -16.201            14.5        0.043394        0.055983
v  Velocity[Z]             -25.673          11.719         -1.6651        -0.49598
v  ǁVelocityǁ         0.00047918          25.861           6.299           5.088
v  Pressure                -550.52          178.28          9.5839          23.494
v  k                   6.1989e-014          9.4312       0.0079806       0.0082346
v  omega                    6.1628      2.732e+008       1.29e+006           75593
v  TempK                    298.13          363.17          309.47          312.78
v  TurbVisc            3.3686e-021      0.00023478     2.9509e-006     1.0879e-005
v  CourantNb           3.8985e-005          1.2772         0.76492         0.97222
v  FourierNb             0.0030967               1         0.38026        0.076316
v  total_pressure      1.0077e+005      1.015e+005     1.0133e+005     1.0135e+005
v  Local Time Step          1e-006        0.007908       0.0001018      0.00027948

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.38          305.46
v  Yplus               0          2.9549         0.54755         0.38072


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.23102               2          1.1452          1.0485


 INSTANT    0.108000000E-02   TIME STEP NUMBER             108
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924779E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.27020E-01 0.47161E+01
   Friction velocity        uk    :  0.27020E-01 0.47122E+01
   Dimensionless distance   yplus :  0.19371E-01 0.29541E+01
   Friction thermal sca.    tstar : -0.23002E-03 0.65914E+02
   Rough dim-less th. sca.  tplus :  0.13722E-01 0.20927E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18671E+00      11   0.53307E-05   0.47144E+02 0.18504E+03 
c  Velocity[X]                                      0.23182E+02 
c  Velocity[Y]                                      0.43561E+01 
c  Velocity[Z]                                      0.19606E+02 
c  Pressure     0.37528E-04      24   0.11071E-02   0.48894E-01 0.10537E+03 
c  k            0.29771E-03      13   0.13931E-03   0.27522E-02 0.51733E+03 
c  omega        0.27925E+07       1   0.49587E-06   0.19130E+09 0.25063E+01 
c  TempK        0.69693E+04       8   0.43205E-05   0.11231E+04 0.22230E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -7.3887e-015                             1
a  omega          
a  TempK          
a  Local Time Step     7.8273e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.999          20.202      -0.0039942      -0.0021189
v  Velocity[Y]              -16.17          14.432        0.043784        0.056513
v  Velocity[Z]             -25.666          10.841         -1.6654        -0.49573
v  ǁVelocityǁ         0.00020651          25.852          6.3118          5.0981
v  Pressure                -546.58          178.95          10.133          23.985
v  k                   7.3887e-015          9.2245        0.008169       0.0083736
v  omega                    6.3015      2.732e+008       1.29e+006           75603
v  TempK                    298.13          363.17          309.63          312.82
v  TurbVisc            1.5619e-021      0.00023256     2.9851e-006     1.0983e-005
v  CourantNb           3.6278e-005          1.2776         0.76511         0.97224
v  FourierNb             0.0030904               1         0.38028        0.076422
v  total_pressure      1.0078e+005      1.015e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0081235      0.00010151      0.00027873

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.38          305.46
v  Yplus               0          2.9541         0.54802         0.38179


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.34326               2          1.1454          1.0487


 INSTANT    0.109000000E-02   TIME STEP NUMBER             109
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924669E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18876E-01 0.47144E+01
   Friction velocity        uk    :  0.18876E-01 0.47105E+01
   Dimensionless distance   yplus :  0.13531E-01 0.29533E+01
   Friction thermal sca.    tstar : -0.48714E-03 0.71096E+02
   Rough dim-less th. sca.  tplus :  0.95856E-02 0.20921E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18712E+00      11   0.53369E-05   0.46879E+02 0.18373E+03 
c  Velocity[X]                                      0.23026E+02 
c  Velocity[Y]                                      0.43403E+01 
c  Velocity[Z]                                      0.19513E+02 
c  Pressure     0.37596E-04      24   0.10686E-02   0.48811E-01 0.10474E+03 
c  k            0.30104E-03      13   0.15151E-03   0.29487E-02 0.51945E+03 
c  omega        0.27925E+07       1   0.49364E-06   0.17441E+09 0.24099E+01 
c  TempK        0.69810E+04       8   0.43462E-05   0.11088E+04 0.22357E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -7.2142e-014                             1
a  omega          
a  TempK          
a  Local Time Step     7.8249e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.876           20.12      -0.0039103      -0.0022486
v  Velocity[Y]             -16.139           14.52        0.044161        0.057032
v  Velocity[Z]             -25.659          10.545         -1.6657        -0.49548
v  ǁVelocityǁ         0.00013405          25.844          6.3246          5.1081
v  Pressure                -542.13          179.63          10.683          24.478
v  k                   7.2142e-014          8.9771        0.008361       0.0085202
v  omega                    6.4431      2.732e+008       1.29e+006           75613
v  TempK                    298.13          363.17          309.79          312.86
v  TurbVisc            1.8616e-022      0.00022927     3.0204e-006     1.1094e-005
v  CourantNb           3.1978e-005           1.278          0.7653         0.97226
v  FourierNb             0.0030841               1         0.38029        0.076554
v  total_pressure      1.0078e+005      1.015e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0083889      0.00010124      0.00027801

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.38          305.46
v  Yplus               0          2.9533         0.54848         0.38283


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.21053               2          1.1456          1.0488


 INSTANT    0.110000000E-02   TIME STEP NUMBER             110
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924743E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10997E-01 0.47127E+01
   Friction velocity        uk    :  0.10997E-01 0.47087E+01
   Dimensionless distance   yplus :  0.78830E-02 0.29527E+01
   Friction thermal sca.    tstar : -0.46753E-03 0.12316E+03
   Rough dim-less th. sca.  tplus :  0.55844E-02 0.20917E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18753E+00      11   0.53455E-05   0.46617E+02 0.18243E+03 
c  Velocity[X]                                      0.22868E+02 
c  Velocity[Y]                                      0.43257E+01 
c  Velocity[Z]                                      0.19423E+02 
c  Pressure     0.37839E-04      24   0.10526E-02   0.48957E-01 0.10786E+03 
c  k            0.30449E-03      13   0.16415E-03   0.31577E-02 0.52124E+03 
c  omega        0.27925E+07       1   0.49343E-06   0.18121E+09 0.24232E+01 
c  TempK        0.69927E+04       8   0.43692E-05   0.10946E+04 0.22482E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -3.1124e-008                             3
a  omega          
a  TempK          
a  Local Time Step     7.8221e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.795          20.041      -0.0038236      -0.0023766
v  Velocity[Y]             -16.192          15.495        0.044533        0.057543
v  Velocity[Z]             -25.652          10.537          -1.666        -0.49524
v  ǁVelocityǁ          0.0002048          25.836          6.3372          5.1182
v  Pressure                -538.29          180.34          11.264              25
v  k                   1.3158e-013          8.6851       0.0085566       0.0086752
v  omega                     6.588      2.732e+008       1.29e+006           75623
v  TempK                    298.13          363.17          309.96           312.9
v  TurbVisc            1.8177e-021      0.00022497     3.0571e-006     1.1214e-005
v  CourantNb           2.6956e-005          1.2784         0.76549         0.97229
v  FourierNb             0.0030779               1         0.38032        0.076712
v  total_pressure      1.0079e+005     1.0151e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0085367      0.00010097      0.00027731

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.39          305.46
v  Yplus               0          2.9527         0.54894         0.38385


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.30216               2          1.1458           1.049


 INSTANT    0.111000000E-02   TIME STEP NUMBER             111
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924778E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14042E-01 0.47108E+01
   Friction velocity        uk    :  0.14042E-01 0.47068E+01
   Dimensionless distance   yplus :  0.10066E-01 0.29519E+01
   Friction thermal sca.    tstar : -0.26462E-03 0.98667E+02
   Rough dim-less th. sca.  tplus :  0.71311E-02 0.20911E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18795E+00      11   0.53580E-05   0.46365E+02 0.18117E+03 
c  Velocity[X]                                      0.22716E+02 
c  Velocity[Y]                                      0.43166E+01 
c  Velocity[Z]                                      0.19333E+02 
c  Pressure     0.38143E-04      23   0.10183E-02   0.49176E-01 0.10595E+03 
c  k            0.30805E-03      13   0.17394E-03   0.33821E-02 0.52108E+03 
c  omega        0.27925E+07       1   0.49303E-06   0.18895E+09 0.24454E+01 
c  TempK        0.70045E+04       8   0.43882E-05   0.10804E+04 0.22602E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -1.28e-007                             4
a  omega          
a  TempK          
a  Local Time Step     7.8202e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.734          19.965      -0.0037379      -0.0025043
v  Velocity[Y]             -16.426          14.462        0.044884        0.058051
v  Velocity[Z]             -25.645          10.621         -1.6664        -0.49499
v  ǁVelocityǁ         0.00036674          25.829          6.3496          5.1282
v  Pressure                -534.65          181.04          11.833          25.511
v  k                   1.1503e-013          8.3385       0.0087559        0.008839
v  omega                    6.7363     2.7321e+008       1.29e+006           75632
v  TempK                    298.13          363.17          310.12          312.94
v  TurbVisc            3.3152e-021      0.00022307     3.0952e-006     1.1343e-005
v  CourantNb           2.3324e-005          1.2787         0.76567         0.97232
v  FourierNb             0.0030717               1         0.38035        0.076895
v  total_pressure      1.0079e+005     1.0151e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0083271       0.0001007      0.00027661

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.39          305.46
v  Yplus               0          2.9519          0.5494         0.38486


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.3301               2           1.146          1.0492


 INSTANT    0.112000000E-02   TIME STEP NUMBER             112
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924683E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16000E-01 0.47088E+01
   Friction velocity        uk    :  0.16000E-01 0.47048E+01
   Dimensionless distance   yplus :  0.11468E-01 0.29512E+01
   Friction thermal sca.    tstar : -0.25229E-03 0.92213E+02
   Rough dim-less th. sca.  tplus :  0.81238E-02 0.20906E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18836E+00      11   0.53724E-05   0.46090E+02 0.17987E+03 
c  Velocity[X]                                      0.22555E+02 
c  Velocity[Y]                                      0.42938E+01 
c  Velocity[Z]                                      0.19240E+02 
c  Pressure     0.37793E-04      24   0.10084E-02   0.48553E-01 0.10281E+03 
c  k            0.31174E-03      13   0.19778E-03   0.36365E-02 0.51863E+03 
c  omega        0.27925E+07       1   0.49095E-06   0.17549E+09 0.23680E+01 
c  TempK        0.70162E+04       8   0.44024E-05   0.10663E+04 0.22714E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.0348e-007                             6
a  omega          
a  TempK          
a  Local Time Step     7.8189e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -19.67          19.893      -0.0036468      -0.0026343
v  Velocity[Y]             -16.243          14.393        0.045238        0.058581
v  Velocity[Z]             -25.639          10.672         -1.6667        -0.49473
v  ǁVelocityǁ         0.00042126          25.822          6.3619          5.1382
v  Pressure                -531.35          181.72          12.381          26.002
v  k                   4.8857e-014          7.9283       0.0089586       0.0090122
v  omega                    6.8883     2.7321e+008       1.29e+006           75642
v  TempK                    298.13          363.17          310.28          312.98
v  TurbVisc            2.9169e-021      0.00024371     3.1348e-006     1.1481e-005
v  CourantNb           2.4185e-005           1.279         0.76586         0.97233
v  FourierNb             0.0030654               1         0.38039        0.077098
v  total_pressure      1.0079e+005     1.0151e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0085245      0.00010044      0.00027589

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.39          305.46
v  Yplus               0          2.9512         0.54986         0.38586


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.32329               2          1.1462          1.0494


 INSTANT    0.113000000E-02   TIME STEP NUMBER             113
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924711E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.19484E-01 0.47069E+01
   Friction velocity        uk    :  0.19484E-01 0.47029E+01
   Dimensionless distance   yplus :  0.13965E-01 0.29506E+01
   Friction thermal sca.    tstar : -0.32615E-03 0.76297E+02
   Rough dim-less th. sca.  tplus :  0.98930E-02 0.20902E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18877E+00      11   0.53865E-05   0.45807E+02 0.17859E+03 
c  Velocity[X]                                      0.22399E+02 
c  Velocity[Y]                                      0.42641E+01 
c  Velocity[Z]                                      0.19143E+02 
c  Pressure     0.37464E-04      24   0.10069E-02   0.47974E-01 0.99554E+02 
c  k            0.31557E-03      13   0.21230E-03   0.37814E-02 0.51224E+03 
c  omega        0.27925E+07       1   0.48938E-06   0.15947E+09 0.22796E+01 
c  TempK        0.70280E+04       8   0.44113E-05   0.10522E+04 0.22815E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.1273e-007                             7
a  omega          
a  TempK          
a  Local Time Step     7.8181e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.599          19.824      -0.0035593      -0.0027794
v  Velocity[Y]             -16.195          14.352        0.045581        0.059118
v  Velocity[Z]             -25.634          10.713          -1.667        -0.49448
v  ǁVelocityǁ         0.00049552          25.817          6.3741          5.1483
v  Pressure                -528.95          182.36          12.904          26.468
v  k                   3.8132e-015          7.4626       0.0091645       0.0091953
v  omega                    7.0442     2.7321e+008       1.29e+006           75652
v  TempK                    298.13          363.17          310.45          313.02
v  TurbVisc             1.239e-021      0.00024897     3.1758e-006     1.1628e-005
v  CourantNb           2.4049e-005          1.2791         0.76604         0.97234
v  FourierNb              0.003059               1         0.38043        0.077321
v  total_pressure       1.008e+005     1.0151e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006        0.009377      0.00010018      0.00027516

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           303.4          305.46
v  Yplus               0          2.9506         0.55031         0.38683


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.3431               2          1.1465          1.0497


 INSTANT    0.114000000E-02   TIME STEP NUMBER             114
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924748E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.21155E-01 0.47049E+01
   Friction velocity        uk    :  0.21155E-01 0.47009E+01
   Dimensionless distance   yplus :  0.15180E-01 0.29499E+01
   Friction thermal sca.    tstar : -0.41667E-03 0.62501E+02
   Rough dim-less th. sca.  tplus :  0.10753E-01 0.20898E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18919E+00      11   0.54092E-05   0.45524E+02 0.17732E+03 
c  Velocity[X]                                      0.22250E+02 
c  Velocity[Y]                                      0.42405E+01 
c  Velocity[Z]                                      0.19033E+02 
c  Pressure     0.37544E-04      24   0.99368E-03   0.47923E-01 0.98429E+02 
c  k            0.31955E-03      13   0.22969E-03   0.39368E-02 0.50393E+03 
c  omega        0.27925E+07       1   0.48912E-06   0.15708E+09 0.22658E+01 
c  TempK        0.70398E+04       8   0.44145E-05   0.10380E+04 0.22903E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.0395e-007                             8
a  omega          
a  TempK          
a  Local Time Step     7.8183e-007        0.010051             2             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.533          19.758      -0.0034725       -0.002935
v  Velocity[Y]             -16.184          14.374         0.04592        0.059656
v  Velocity[Z]             -25.628          10.761         -1.6673        -0.49422
v  ǁVelocityǁ         0.00064986          25.811          6.3862          5.1583
v  Pressure                 -526.9             183          13.419          26.926
v  k                   2.0687e-015           6.927       0.0093734       0.0093891
v  omega                    7.2042     2.7321e+008       1.29e+006           75662
v  TempK                    298.13          363.17          310.61          313.06
v  TurbVisc              9.67e-023      0.00026355     3.2184e-006     1.1785e-005
v  CourantNb           2.6291e-005          1.2791         0.76622         0.97234
v  FourierNb             0.0030525               1         0.38048        0.077566
v  total_pressure       1.008e+005     1.0151e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006            0.01     9.9924e-005      0.00027441

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           303.4          305.46
v  Yplus               0          2.9499         0.55076         0.38779


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.25383               2          1.1467          1.0499


 INSTANT    0.115000000E-02   TIME STEP NUMBER             115
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924694E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.27939E-01 0.47029E+01
   Friction velocity        uk    :  0.27939E-01 0.46989E+01
   Dimensionless distance   yplus :  0.20026E-01 0.29494E+01
   Friction thermal sca.    tstar : -0.50825E-03 0.55812E+02
   Rough dim-less th. sca.  tplus :  0.14186E-01 0.20893E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.18960E+00      11   0.54258E-05   0.45233E+02 0.17604E+03 
c  Velocity[X]                                      0.22100E+02 
c  Velocity[Y]                                      0.42121E+01 
c  Velocity[Z]                                      0.18921E+02 
c  Pressure     0.37399E-04      25   0.98803E-03   0.47586E-01 0.98477E+02 
c  k            0.32370E-03      13   0.24668E-03   0.41483E-02 0.49567E+03 
c  omega        0.27925E+07       1   0.49006E-06   0.16791E+09 0.23128E+01 
c  TempK        0.70517E+04       8   0.44115E-05   0.10238E+04 0.22978E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.1253e-007                             7
a  omega          
a  TempK          
a  Local Time Step     7.8192e-007        0.010496             2             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.493          19.696      -0.0033915      -0.0030758
v  Velocity[Y]             -16.246          15.368        0.046254        0.060184
v  Velocity[Z]             -25.623          10.825         -1.6677        -0.49395
v  ǁVelocityǁ         0.00064668          25.806          6.3982          5.1683
v  Pressure                -524.68          183.65          13.937          27.387
v  k                   5.9047e-014          6.3018       0.0095852       0.0095938
v  omega                    7.3683     2.7321e+008       1.29e+006           75671
v  TempK                    298.13          363.17          310.77          313.09
v  TurbVisc            5.2459e-023      0.00027921     3.2629e-006     1.1953e-005
v  CourantNb           3.1116e-005          1.2789          0.7664         0.97233
v  FourierNb              0.003046               1         0.38053        0.077828
v  total_pressure       1.008e+005     1.0151e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006            0.01     9.9669e-005      0.00027363

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.41          305.46
v  Yplus               0          2.9494         0.55121         0.38873


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.31797               2          1.1469          1.0502


 INSTANT    0.116000000E-02   TIME STEP NUMBER             116
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924823E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.29153E-01 0.47010E+01
   Friction velocity        uk    :  0.29153E-01 0.46971E+01
   Dimensionless distance   yplus :  0.20898E-01 0.29487E+01
   Friction thermal sca.    tstar : -0.59861E-03 0.53828E+02
   Rough dim-less th. sca.  tplus :  0.14804E-01 0.20889E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19002E+00      11   0.54608E-05   0.44951E+02 0.17478E+03 
c  Velocity[X]                                      0.21945E+02 
c  Velocity[Y]                                      0.41895E+01 
c  Velocity[Z]                                      0.18817E+02 
c  Pressure     0.37218E-04      23   0.95942E-03   0.47211E-01 0.92872E+02 
c  k            0.32804E-03      13   0.25361E-03   0.43648E-02 0.48675E+03 
c  omega        0.27925E+07       1   0.49057E-06   0.17016E+09 0.23380E+01 
c  TempK        0.70636E+04       8   0.44023E-05   0.10097E+04 0.23038E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.0374e-007                             8
a  omega          
a  TempK          
a  Local Time Step     7.8217e-007        0.010813             2             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.455          19.645      -0.0033141      -0.0032117
v  Velocity[Y]             -16.302          14.412        0.046578        0.060704
v  Velocity[Z]             -25.617          10.875          -1.668        -0.49366
v  ǁVelocityǁ         0.00047744          25.801            6.41          5.1784
v  Pressure                -522.81          184.26          14.414          27.806
v  k                   3.9499e-014          6.0935       0.0097997       0.0098097
v  omega                    7.5367     2.7321e+008       1.29e+006           75681
v  TempK                    298.12          363.17          310.93          313.13
v  TurbVisc            1.4974e-021      0.00028791     3.3093e-006     1.2132e-005
v  CourantNb            3.697e-005          1.2785         0.76658         0.97233
v  FourierNb             0.0030396               1         0.38058        0.078109
v  total_pressure       1.008e+005     1.0151e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006            0.01     9.9416e-005      0.00027285

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.41          305.46
v  Yplus               0          2.9487         0.55164         0.38965


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.31399               2          1.1472          1.0504


 INSTANT    0.117000000E-02   TIME STEP NUMBER             117
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924680E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.25845E-01 0.46992E+01
   Friction velocity        uk    :  0.25845E-01 0.46952E+01
   Dimensionless distance   yplus :  0.18526E-01 0.29481E+01
   Friction thermal sca.    tstar : -0.68587E-03 0.57490E+02
   Rough dim-less th. sca.  tplus :  0.13124E-01 0.20885E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19043E+00      11   0.54814E-05   0.44660E+02 0.17349E+03 
c  Velocity[X]                                      0.21792E+02 
c  Velocity[Y]                                      0.41565E+01 
c  Velocity[Z]                                      0.18712E+02 
c  Pressure     0.37187E-04      23   0.95984E-03   0.47033E-01 0.89085E+02 
c  k            0.33261E-03      14   0.25183E-03   0.45813E-02 0.47636E+03 
c  omega        0.27925E+07       1   0.48933E-06   0.15714E+09 0.22692E+01 
c  TempK        0.70756E+04       8   0.43871E-05   0.99554E+03 0.23084E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.0627e-007                             9
a  omega          
a  TempK          
a  Local Time Step     7.8254e-007         0.01004             2             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.418          19.603      -0.0032398       -0.003342
v  Velocity[Y]             -16.253          14.357        0.046895        0.061213
v  Velocity[Z]              -25.61          10.921         -1.6683        -0.49336
v  ǁVelocityǁ         0.00028619          25.796          6.4217          5.1884
v  Pressure                   -521          184.84          14.866          28.201
v  k                    5.786e-014          6.1131        0.010017        0.010037
v  omega                    7.7093     2.7321e+008       1.29e+006           75691
v  TempK                    298.11          363.17          311.09          313.17
v  TurbVisc            9.9685e-022      0.00029689     3.3572e-006     1.2321e-005
v  CourantNb           4.2569e-005          1.2779         0.76676         0.97233
v  FourierNb             0.0030331               1         0.38063        0.078397
v  total_pressure       1.008e+005     1.0151e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006            0.01     9.9167e-005      0.00027206

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.41          305.46
v  Yplus               0          2.9481         0.55206         0.39055


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.3508               2          1.1474          1.0507


 INSTANT    0.118000000E-02   TIME STEP NUMBER             118
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924726E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.21723E-01 0.46975E+01
   Friction velocity        uk    :  0.21723E-01 0.46935E+01
   Dimensionless distance   yplus :  0.15572E-01 0.29475E+01
   Friction thermal sca.    tstar : -0.76738E-03 0.69484E+02
   Rough dim-less th. sca.  tplus :  0.11031E-01 0.20880E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19085E+00      11   0.55061E-05   0.44387E+02 0.17224E+03 
c  Velocity[X]                                      0.21653E+02 
c  Velocity[Y]                                      0.41228E+01 
c  Velocity[Z]                                      0.18611E+02 
c  Pressure     0.37112E-04      22   0.94133E-03   0.46801E-01 0.87811E+02 
c  k            0.33744E-03      14   0.24401E-03   0.47989E-02 0.46479E+03 
c  omega        0.27925E+07       1   0.48924E-06   0.15333E+09 0.22543E+01 
c  TempK        0.70876E+04       8   0.43660E-05   0.98145E+03 0.23114E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.3087e-007                            13
a  omega          
a  TempK          
a  Local Time Step     7.8303e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.381          19.562       -0.003172      -0.0034755
v  Velocity[Y]             -16.228           14.33        0.047205        0.061709
v  Velocity[Z]             -25.604          10.943         -1.6687        -0.49306
v  ǁVelocityǁ         0.00016727          25.792          6.4333          5.1985
v  Pressure                -518.97          185.41          15.313          28.591
v  k                   4.8054e-015          6.1328        0.010237        0.010276
v  omega                    7.8864     2.7322e+008       1.29e+006           75700
v  TempK                     298.1          363.17          311.25          313.21
v  TurbVisc            1.4602e-021      0.00031219     3.4069e-006      1.252e-005
v  CourantNb           4.2645e-005          1.2771         0.76693         0.97232
v  FourierNb             0.0030266               1         0.38069        0.078695
v  total_pressure      1.0081e+005     1.0151e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0091311     9.8916e-005      0.00027123

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.42          305.46
v  Yplus               0          2.9475         0.55248         0.39143


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42643               2          1.1476           1.051


 INSTANT    0.119000000E-02   TIME STEP NUMBER             119
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924702E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15676E-01 0.46959E+01
   Friction velocity        uk    :  0.15676E-01 0.46919E+01
   Dimensionless distance   yplus :  0.11237E-01 0.29470E+01
   Friction thermal sca.    tstar : -0.83919E-03 0.95473E+02
   Rough dim-less th. sca.  tplus :  0.79606E-02 0.20876E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19127E+00      11   0.55537E-05   0.44117E+02 0.17099E+03 
c  Velocity[X]                                      0.21523E+02 
c  Velocity[Y]                                      0.40903E+01 
c  Velocity[Z]                                      0.18504E+02 
c  Pressure     0.37202E-04      22   0.93937E-03   0.46780E-01 0.87126E+02 
c  k            0.34255E-03      14   0.23621E-03   0.49934E-02 0.45177E+03 
c  omega        0.27925E+07       1   0.48904E-06   0.14789E+09 0.22318E+01 
c  TempK        0.70996E+04       8   0.43392E-05   0.96739E+03 0.23130E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.1066e-007                            12
a  omega          
a  TempK          
a  Local Time Step     7.8369e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.344          19.522      -0.0031142       -0.003616
v  Velocity[Y]             -16.217          14.355        0.047505        0.062192
v  Velocity[Z]               -25.6          10.937         -1.6691        -0.49276
v  ǁVelocityǁ         0.00023849          25.787          6.4448          5.2086
v  Pressure                -516.65          185.99          15.758          28.979
v  k                   1.1089e-013          6.3085        0.010459        0.010526
v  omega                    7.9944     2.7322e+008       1.29e+006           75710
v  TempK                    298.09          363.17          311.41          313.24
v  TurbVisc            1.2107e-022      0.00032063     3.4589e-006     1.2729e-005
v  CourantNb            3.861e-005           1.276          0.7671         0.97231
v  FourierNb               0.00302               1         0.38075        0.079006
v  total_pressure      1.0081e+005     1.0151e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0083238     9.8663e-005      0.00027037

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.42          305.46
v  Yplus               0           2.947         0.55289         0.39228


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41874               2          1.1479          1.0513


 INSTANT    0.120000000E-02   TIME STEP NUMBER             120
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924709E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16499E-01 0.46943E+01
   Friction velocity        uk    :  0.16499E-01 0.46903E+01
   Dimensionless distance   yplus :  0.11827E-01 0.29464E+01
   Friction thermal sca.    tstar : -0.89894E-03 0.92845E+02
   Rough dim-less th. sca.  tplus :  0.83784E-02 0.20873E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19168E+00      11   0.55887E-05   0.43848E+02 0.16976E+03 
c  Velocity[X]                                      0.21384E+02 
c  Velocity[Y]                                      0.40560E+01 
c  Velocity[Z]                                      0.18408E+02 
c  Pressure     0.37169E-04      22   0.92466E-03   0.46604E-01 0.85694E+02 
c  k            0.34794E-03      14   0.22571E-03   0.51424E-02 0.43752E+03 
c  omega        0.27925E+07       1   0.48965E-06   0.15747E+09 0.22616E+01 
c  TempK        0.71117E+04       8   0.43072E-05   0.95338E+03 0.23130E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -8.3942e-008                            12
a  omega          
a  TempK          
a  Local Time Step     7.8443e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.307          19.483      -0.0030622      -0.0037699
v  Velocity[Y]             -16.273          15.344         0.04781         0.06266
v  Velocity[Z]             -25.596          11.161         -1.6695        -0.49246
v  ǁVelocityǁ         0.00039978          25.783          6.4562          5.2188
v  Pressure                -514.46          186.55          16.193          29.355
v  k                   9.2132e-014          6.4284        0.010684        0.010789
v  omega                    8.1018     2.7322e+008       1.29e+006           75719
v  TempK                    298.08          363.17          311.56          313.28
v  TurbVisc            2.7985e-021      0.00032906     3.5128e-006     1.2948e-005
v  CourantNb           3.4756e-005          1.2748         0.76727         0.97229
v  FourierNb             0.0030134               1         0.38082        0.079333
v  total_pressure      1.0081e+005     1.0151e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0076265     9.8411e-005      0.00026951

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.43          305.46
v  Yplus               0          2.9464          0.5533         0.39313


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.32685               2          1.1481          1.0516


 INSTANT    0.121000000E-02   TIME STEP NUMBER             121
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924792E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.21707E-01 0.46929E+01
   Friction velocity        uk    :  0.21707E-01 0.46889E+01
   Dimensionless distance   yplus :  0.15561E-01 0.29459E+01
   Friction thermal sca.    tstar : -0.94307E-03 0.95030E+02
   Rough dim-less th. sca.  tplus :  0.11023E-01 0.20869E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19210E+00      11   0.56236E-05   0.43582E+02 0.16854E+03 
c  Velocity[X]                                      0.21245E+02 
c  Velocity[Y]                                      0.40264E+01 
c  Velocity[Z]                                      0.18311E+02 
c  Pressure     0.36885E-04      22   0.91312E-03   0.46119E-01 0.81796E+02 
c  k            0.35361E-03      14   0.22513E-03   0.53352E-02 0.42307E+03 
c  omega        0.27925E+07       1   0.48946E-06   0.16072E+09 0.22628E+01 
c  TempK        0.71239E+04       8   0.42704E-05   0.93943E+03 0.23117E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -8.5638e-007                            13
a  omega          
a  TempK          
a  Local Time Step     7.8534e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -19.27          19.445      -0.0030089      -0.0039122
v  Velocity[Y]              -16.34           14.46        0.048104        0.063115
v  Velocity[Z]             -25.591          13.015         -1.6699        -0.49217
v  ǁVelocityǁ         0.00057331          25.778          6.4674          5.2289
v  Pressure                 -512.5          187.08          16.596            29.7
v  k                   1.0244e-013          6.5145        0.010913        0.011065
v  omega                    8.2098     2.7322e+008     1.2901e+006           75729
v  TempK                    298.07          363.17          311.72          313.31
v  TurbVisc            2.3251e-021      0.00033427      3.569e-006     1.3176e-005
v  CourantNb            3.211e-005          1.2733         0.76744         0.97228
v  FourierNb             0.0030068               1          0.3809        0.079674
v  total_pressure      1.0081e+005     1.0151e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0071042     9.8165e-005      0.00026866

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.43          305.46
v  Yplus               0          2.9459         0.55372         0.39397


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.26076               2          1.1483          1.0519


 INSTANT    0.122000000E-02   TIME STEP NUMBER             122
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924760E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.26562E-01 0.46916E+01
   Friction velocity        uk    :  0.26562E-01 0.46876E+01
   Dimensionless distance   yplus :  0.19041E-01 0.29454E+01
   Friction thermal sca.    tstar : -0.96881E-03 0.14396E+03
   Rough dim-less th. sca.  tplus :  0.13488E-01 0.20865E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19252E+00      11   0.56718E-05   0.43303E+02 0.16728E+03 
c  Velocity[X]                                      0.21111E+02 
c  Velocity[Y]                                      0.39886E+01 
c  Velocity[Z]                                      0.18204E+02 
c  Pressure     0.36972E-04      21   0.89235E-03   0.46100E-01 0.77808E+02 
c  k            0.35956E-03      14   0.22974E-03   0.55674E-02 0.40860E+03 
c  omega        0.27925E+07       1   0.48822E-06   0.15065E+09 0.21985E+01 
c  TempK        0.71361E+04       8   0.42293E-05   0.92561E+03 0.23090E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -4.1504e-007                            13
a  omega          
a  TempK          
a  Local Time Step     7.8643e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.232          19.408       -0.002954      -0.0040501
v  Velocity[Y]             -16.279          14.415        0.048405        0.063567
v  Velocity[Z]             -25.587           11.76         -1.6703        -0.49188
v  ǁVelocityǁ         0.00074562          25.774          6.4786          5.2391
v  Pressure                -510.35          187.58          16.969          30.013
v  k                   3.2852e-014          6.5855        0.011144        0.011353
v  omega                    8.3183     2.7322e+008     1.2901e+006           75738
v  TempK                    298.07          363.17          311.87          313.35
v  TurbVisc            2.5853e-021      0.00033899     3.6275e-006     1.3414e-005
v  CourantNb           2.9732e-005          1.2716         0.76761         0.97227
v  FourierNb             0.0030002               1         0.38098        0.080024
v  total_pressure      1.0081e+005     1.0151e+005     1.0134e+005     1.0136e+005
v  Local Time Step          1e-006       0.0071044     9.7922e-005      0.00026779

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.44          305.47
v  Yplus               0          2.9454         0.55413          0.3948


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.355               2          1.1486          1.0523


 INSTANT    0.123000000E-02   TIME STEP NUMBER             123
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924761E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.30687E-01 0.46904E+01
   Friction velocity        uk    :  0.30687E-01 0.46864E+01
   Dimensionless distance   yplus :  0.21998E-01 0.29450E+01
   Friction thermal sca.    tstar : -0.97491E-03 0.87242E+02
   Rough dim-less th. sca.  tplus :  0.15583E-01 0.20862E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19294E+00      11   0.57526E-05   0.43025E+02 0.16603E+03 
c  Velocity[X]                                      0.20984E+02 
c  Velocity[Y]                                      0.39502E+01 
c  Velocity[Z]                                      0.18090E+02 
c  Pressure     0.36528E-04      23   0.88803E-03   0.45429E-01 0.78125E+02 
c  k            0.36582E-03      14   0.23842E-03   0.57958E-02 0.39306E+03 
c  omega        0.27925E+07       1   0.48643E-06   0.13614E+09 0.20963E+01 
c  TempK        0.71483E+04       8   0.41843E-05   0.91196E+03 0.23050E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -4.0686e-007                            14
a  omega          
a  TempK          
a  Local Time Step     7.8766e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.194          19.371      -0.0029026      -0.0041937
v  Velocity[Y]             -16.217          14.387          0.0487        0.064013
v  Velocity[Z]             -25.583          10.791         -1.6708        -0.49162
v  ǁVelocityǁ         0.00084726           25.77          6.4896          5.2492
v  Pressure                -509.13          188.09           17.35          30.335
v  k                   1.5358e-014          6.6547        0.011377        0.011653
v  omega                    8.4274     2.7322e+008     1.2901e+006           75748
v  TempK                    298.06          363.17          312.03          313.39
v  TurbVisc            8.3352e-022      0.00034282     3.6882e-006     1.3661e-005
v  CourantNb           2.7206e-005          1.2696         0.76778         0.97227
v  FourierNb             0.0029937               1         0.38106        0.080391
v  total_pressure      1.0082e+005     1.0151e+005     1.0134e+005     1.0136e+005
v  Local Time Step          1e-006       0.0072511     9.7688e-005      0.00026694

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.44          305.47
v  Yplus               0           2.945         0.55455         0.39562


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40597               2          1.1488          1.0527


 INSTANT    0.124000000E-02   TIME STEP NUMBER             124
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924833E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.31744E-01 0.46893E+01
   Friction velocity        uk    :  0.31744E-01 0.46853E+01
   Dimensionless distance   yplus :  0.22758E-01 0.29445E+01
   Friction thermal sca.    tstar : -0.96210E-03 0.63722E+02
   Rough dim-less th. sca.  tplus :  0.16122E-01 0.20859E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19336E+00      11   0.58336E-05   0.42749E+02 0.16479E+03 
c  Velocity[X]                                      0.20855E+02 
c  Velocity[Y]                                      0.39160E+01 
c  Velocity[Z]                                      0.17979E+02 
c  Pressure     0.36399E-04      22   0.88872E-03   0.45157E-01 0.76772E+02 
c  k            0.37240E-03      14   0.24903E-03   0.60006E-02 0.37712E+03 
c  omega        0.27925E+07       1   0.48623E-06   0.13456E+09 0.20788E+01 
c  TempK        0.71606E+04       8   0.41361E-05   0.89847E+03 0.22998E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -4.1138e-008                            17
a  omega          
a  TempK          
a  Local Time Step     7.8906e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.154          19.336      -0.0028586      -0.0043496
v  Velocity[Y]             -16.205          14.383        0.048992         0.06444
v  Velocity[Z]              -25.58          10.736         -1.6712        -0.49136
v  ǁVelocityǁ          0.0007358          25.767          6.5005          5.2594
v  Pressure                   -509           188.6          17.724          30.651
v  k                   5.7202e-014           6.732        0.011612        0.011968
v  omega                     8.537     2.7322e+008     1.2901e+006           75757
v  TempK                    298.06          363.17          312.18          313.42
v  TurbVisc            5.1169e-022      0.00035153     3.7508e-006     1.3915e-005
v  CourantNb           2.4869e-005          1.2673         0.76795         0.97226
v  FourierNb             0.0029872               1         0.38115        0.080765
v  total_pressure      1.0082e+005     1.0151e+005     1.0134e+005     1.0136e+005
v  Local Time Step          1e-006       0.0072094     9.7461e-005       0.0002661

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.45          305.47
v  Yplus               0          2.9445         0.55497         0.39642


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45602               2          1.1491           1.053


 INSTANT    0.125000000E-02   TIME STEP NUMBER             125
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924675E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.20686E-01 0.46883E+01
   Friction velocity        uk    :  0.20686E-01 0.46843E+01
   Dimensionless distance   yplus :  0.14837E-01 0.29442E+01
   Friction thermal sca.    tstar : -0.92934E-03 0.65718E+02
   Rough dim-less th. sca.  tplus :  0.10510E-01 0.20857E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19378E+00      11   0.58963E-05   0.42471E+02 0.16354E+03 
c  Velocity[X]                                      0.20720E+02 
c  Velocity[Y]                                      0.38761E+01 
c  Velocity[Z]                                      0.17875E+02 
c  Pressure     0.36561E-04      23   0.89894E-03   0.45250E-01 0.74705E+02 
c  k            0.37935E-03      14   0.26081E-03   0.62960E-02 0.36323E+03 
c  omega        0.27925E+07       1   0.48719E-06   0.14274E+09 0.21166E+01 
c  TempK        0.71730E+04       8   0.40852E-05   0.88515E+03 0.22935E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -3.6564e-009                            15
a  omega          
a  TempK          
a  Local Time Step     7.9055e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.123          19.303      -0.0028256      -0.0045256
v  Velocity[Y]             -16.236          15.199        0.049284        0.064852
v  Velocity[Z]             -25.576          10.674         -1.6717        -0.49107
v  ǁVelocityǁ         0.00040258          25.763          6.5113          5.2696
v  Pressure                -508.78          189.09          18.086          30.953
v  k                   4.8943e-014          6.8168         0.01185        0.012296
v  omega                    8.6472     2.7323e+008     1.2901e+006           75767
v  TempK                    298.06          363.17          312.33          313.46
v  TurbVisc            1.4513e-021      0.00036101     3.8156e-006     1.4178e-005
v  CourantNb           2.2475e-005          1.2649         0.76812         0.97226
v  FourierNb             0.0029807               1         0.38125        0.081153
v  total_pressure      1.0082e+005     1.0151e+005     1.0134e+005     1.0136e+005
v  Local Time Step          1e-006       0.0072482      9.724e-005      0.00026528

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.46          305.47
v  Yplus               0          2.9442         0.55538          0.3972


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.30563               2          1.1494          1.0534


 INSTANT    0.126000000E-02   TIME STEP NUMBER             126
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924747E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.20821E-01 0.46875E+01
   Friction velocity        uk    :  0.20821E-01 0.46835E+01
   Dimensionless distance   yplus :  0.14934E-01 0.29438E+01
   Friction thermal sca.    tstar : -0.87571E-03 0.71458E+02
   Rough dim-less th. sca.  tplus :  0.10579E-01 0.20854E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19420E+00      11   0.59922E-05   0.42209E+02 0.16231E+03 
c  Velocity[X]                                      0.20593E+02 
c  Velocity[Y]                                      0.38375E+01 
c  Velocity[Z]                                      0.17778E+02 
c  Pressure     0.36801E-04      22   0.94459E-03   0.45443E-01 0.68954E+02 
c  k            0.38671E-03      15   0.27119E-03   0.67137E-02 0.35191E+03 
c  omega        0.27925E+07       1   0.48786E-06   0.15268E+09 0.21543E+01 
c  TempK        0.71854E+04       8   0.40321E-05   0.87205E+03 0.22861E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -9.6307e-010                            11
a  omega          
a  TempK          
a  Local Time Step     7.9216e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.092          19.274      -0.0028002      -0.0047116
v  Velocity[Y]               -16.3          14.488         0.04957        0.065258
v  Velocity[Z]             -25.572          10.614         -1.6723         -0.4908
v  ǁVelocityǁ         0.00060589          25.759           6.522          5.2798
v  Pressure                -508.42          189.53          18.391          31.198
v  k                   4.4619e-014          6.9162         0.01209        0.012638
v  omega                     8.758     2.7323e+008     1.2901e+006           75776
v  TempK                    298.06          363.17          312.47          313.49
v  TurbVisc            1.2418e-021      0.00037078     3.8839e-006     1.4452e-005
v  CourantNb            2.183e-005          1.2624         0.76828         0.97225
v  FourierNb              0.002974               1         0.38136        0.081562
v  total_pressure      1.0082e+005     1.0151e+005     1.0134e+005     1.0136e+005
v  Local Time Step          1e-006       0.0072442     9.7026e-005      0.00026447

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.46          305.47
v  Yplus               0          2.9438         0.55578         0.39796


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35888               2          1.1496          1.0538


 INSTANT    0.127000000E-02   TIME STEP NUMBER             127
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924799E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.29519E-01 0.46868E+01
   Friction velocity        uk    :  0.29518E-01 0.46828E+01
   Dimensionless distance   yplus :  0.21160E-01 0.29434E+01
   Friction thermal sca.    tstar : -0.80059E-03 0.77459E+02
   Rough dim-less th. sca.  tplus :  0.14990E-01 0.20851E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19463E+00      11   0.59916E-05   0.41938E+02 0.16107E+03 
c  Velocity[X]                                      0.20470E+02 
c  Velocity[Y]                                      0.37891E+01 
c  Velocity[Z]                                      0.17679E+02 
c  Pressure     0.36917E-04      22   0.90101E-03   0.45482E-01 0.64628E+02 
c  k            0.39456E-03      15   0.28691E-03   0.71361E-02 0.34009E+03 
c  omega        0.27925E+07       1   0.48765E-06   0.14769E+09 0.21206E+01 
c  TempK        0.71979E+04       8   0.39772E-05   0.85916E+03 0.22777E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -4.4302e-010                            11
a  omega          
a  TempK          
a  Local Time Step     7.9395e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.059          19.246      -0.0027754       -0.004889
v  Velocity[Y]             -16.251          14.401        0.049855        0.065666
v  Velocity[Z]             -25.569          14.052         -1.6728        -0.49053
v  ǁVelocityǁ          0.0005953          25.755          6.5326          5.2901
v  Pressure                -507.94          189.92          18.657          31.403
v  k                   4.2694e-014          7.0282        0.012332        0.012994
v  omega                    8.8636     2.7323e+008     1.2901e+006           75785
v  TempK                    298.06          363.17          312.62          313.53
v  TurbVisc            1.1321e-021      0.00038048     3.9552e-006     1.4739e-005
v  CourantNb           2.5866e-005          1.2595         0.76844         0.97225
v  FourierNb             0.0029674               1         0.38148        0.081993
v  total_pressure      1.0082e+005     1.0151e+005     1.0134e+005     1.0136e+005
v  Local Time Step          1e-006         0.00724     9.6821e-005      0.00026367

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.47          305.47
v  Yplus               0          2.9434         0.55617          0.3987


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38611               2          1.1499          1.0542


 INSTANT    0.128000000E-02   TIME STEP NUMBER             128
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924823E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.28949E-01 0.46862E+01
   Friction velocity        uk    :  0.28949E-01 0.46822E+01
   Dimensionless distance   yplus :  0.20751E-01 0.29431E+01
   Friction thermal sca.    tstar : -0.70355E-03 0.77325E+02
   Rough dim-less th. sca.  tplus :  0.14700E-01 0.20849E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19505E+00      11   0.60397E-05   0.41671E+02 0.15984E+03 
c  Velocity[X]                                      0.20351E+02 
c  Velocity[Y]                                      0.37371E+01 
c  Velocity[Z]                                      0.17583E+02 
c  Pressure     0.36919E-04      21   0.88744E-03   0.45380E-01 0.63446E+02 
c  k            0.40289E-03      15   0.30523E-03   0.75861E-02 0.32871E+03 
c  omega        0.27925E+07       1   0.48642E-06   0.13087E+09 0.20184E+01 
c  TempK        0.72105E+04       8   0.39212E-05   0.84646E+03 0.22684E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.5973e-010                             8
a  omega          
a  TempK          
a  Local Time Step     7.9587e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -19.024          19.219      -0.0027453      -0.0050584
v  Velocity[Y]             -16.179          14.357        0.050132        0.066068
v  Velocity[Z]             -25.565          10.908         -1.6733        -0.49025
v  ǁVelocityǁ         0.00061709          25.752          6.5431          5.3003
v  Pressure                -507.29           190.3          18.914          31.598
v  k                   3.4834e-014          7.1081        0.012576        0.013366
v  omega                    8.9675     2.7323e+008     1.2901e+006           75795
v  TempK                    298.06          363.17          312.76          313.56
v  TurbVisc            1.0832e-021      0.00039023     4.0285e-006     1.5034e-005
v  CourantNb           3.0599e-005          1.2565          0.7686         0.97224
v  FourierNb             0.0029609               1          0.3816        0.082432
v  total_pressure      1.0082e+005     1.0152e+005     1.0134e+005     1.0136e+005
v  Local Time Step          1e-006       0.0072357     9.6618e-005      0.00026287

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.47          305.47
v  Yplus               0          2.9431         0.55655         0.39943


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.30779               2          1.1502          1.0547


 INSTANT    0.129000000E-02   TIME STEP NUMBER             129
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924636E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.29144E-01 0.46857E+01
   Friction velocity        uk    :  0.29144E-01 0.46817E+01
   Dimensionless distance   yplus :  0.20892E-01 0.29427E+01
   Friction thermal sca.    tstar : -0.57646E-03 0.71960E+02
   Rough dim-less th. sca.  tplus :  0.14800E-01 0.20847E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19548E+00      11   0.61031E-05   0.41383E+02 0.15861E+03 
c  Velocity[X]                                      0.20223E+02 
c  Velocity[Y]                                      0.36896E+01 
c  Velocity[Z]                                      0.17471E+02 
c  Pressure     0.36532E-04      21   0.89251E-03   0.44803E-01 0.62956E+02 
c  k            0.41173E-03      15   0.32507E-03   0.80057E-02 0.31615E+03 
c  omega        0.27925E+07       1   0.48658E-06   0.13302E+09 0.20235E+01 
c  TempK        0.72232E+04       8   0.38645E-05   0.83401E+03 0.22582E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -9.4703e-011                             6
a  omega          
a  TempK          
a  Local Time Step     7.9797e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.988          19.192      -0.0027196      -0.0052234
v  Velocity[Y]             -16.134          14.345        0.050403        0.066458
v  Velocity[Z]             -25.562          10.971         -1.6739        -0.48999
v  ǁVelocityǁ         0.00066741          25.749          6.5534          5.3106
v  Pressure                -506.48          190.68          19.173          31.795
v  k                   2.3375e-014          7.1442        0.012823        0.013753
v  omega                    9.0721     2.7324e+008     1.2901e+006           75804
v  TempK                    298.06          363.17           312.9           313.6
v  TurbVisc            8.8379e-022      0.00040005     4.1061e-006     1.5342e-005
v  CourantNb           2.1393e-005          1.2532         0.76876         0.97223
v  FourierNb             0.0029546               1         0.38173         0.08289
v  total_pressure      1.0082e+005     1.0152e+005     1.0134e+005     1.0136e+005
v  Local Time Step          1e-006       0.0072315     9.6419e-005      0.00026207

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.48          305.47
v  Yplus               0          2.9427         0.55693         0.40015


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.17739               2          1.1505          1.0551


 INSTANT    0.130000000E-02   TIME STEP NUMBER             130
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924726E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.30047E-01 0.46853E+01
   Friction velocity        uk    :  0.30047E-01 0.46813E+01
   Dimensionless distance   yplus :  0.21539E-01 0.29424E+01
   Friction thermal sca.    tstar : -0.41809E-03 0.72404E+02
   Rough dim-less th. sca.  tplus :  0.15258E-01 0.20845E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19591E+00      11   0.61378E-05   0.41082E+02 0.15735E+03 
c  Velocity[X]                                      0.20086E+02 
c  Velocity[Y]                                      0.36430E+01 
c  Velocity[Z]                                      0.17353E+02 
c  Pressure     0.36499E-04      22   0.88877E-03   0.44661E-01 0.62141E+02 
c  k            0.42110E-03      15   0.34614E-03   0.84459E-02 0.30414E+03 
c  omega        0.27925E+07       1   0.48594E-06   0.12842E+09 0.19781E+01 
c  TempK        0.72359E+04       8   0.38075E-05   0.82182E+03 0.22473E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.9543e-011                             3
a  omega          
a  TempK          
a  Local Time Step     8.0014e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.95          19.166      -0.0026931      -0.0053767
v  Velocity[Y]             -16.136          14.686        0.050668        0.066828
v  Velocity[Z]             -25.559          10.996         -1.6744        -0.48973
v  ǁVelocityǁ         0.00060339          25.746          6.5637          5.3208
v  Pressure                -505.54          191.07          19.427          31.987
v  k                   3.3564e-015          7.1259        0.013073        0.014154
v  omega                    9.1776     2.7324e+008     1.2901e+006           75813
v  TempK                    298.06          363.17          313.05          313.63
v  TurbVisc            5.9306e-022      0.00042737     4.1866e-006     1.5661e-005
v  CourantNb           2.8783e-005          1.2498          0.7689         0.97221
v  FourierNb             0.0029486               1         0.38186        0.083362
v  total_pressure      1.0082e+005     1.0152e+005     1.0134e+005     1.0136e+005
v  Local Time Step          1e-006       0.0072273     9.6223e-005      0.00026128

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.48          305.47
v  Yplus               0          2.9424         0.55732         0.40087


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.28343               2          1.1508          1.0556


 INSTANT    0.131000000E-02   TIME STEP NUMBER             131
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924736E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.27572E-01 0.46850E+01
   Friction velocity        uk    :  0.27572E-01 0.46810E+01
   Dimensionless distance   yplus :  0.19776E-01 0.29422E+01
   Friction thermal sca.    tstar : -0.23392E-03 0.72816E+02
   Rough dim-less th. sca.  tplus :  0.14010E-01 0.20843E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19634E+00      11   0.62319E-05   0.40796E+02 0.15611E+03 
c  Velocity[X]                                      0.19954E+02 
c  Velocity[Y]                                      0.36011E+01 
c  Velocity[Z]                                      0.17241E+02 
c  Pressure     0.36560E-04      21   0.87960E-03   0.44639E-01 0.62320E+02 
c  k            0.43097E-03      15   0.36330E-03   0.89699E-02 0.29439E+03 
c  omega        0.27924E+07       1   0.48605E-06   0.13477E+09 0.19875E+01 
c  TempK        0.72488E+04       8   0.37506E-05   0.80991E+03 0.22357E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.0847e-012                             2
a  omega          
a  TempK          
a  Local Time Step     8.0235e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.911           19.14      -0.0026659      -0.0055321
v  Velocity[Y]             -16.243          14.802        0.050928        0.067182
v  Velocity[Z]             -25.556          11.013         -1.6751        -0.48949
v  ǁVelocityǁ         0.00053087          25.742          6.5739          5.3311
v  Pressure                -504.47          191.46          19.688          32.185
v  k                   3.6375e-014          7.0577        0.013326         0.01457
v  omega                    9.2838     2.7324e+008     1.2901e+006           75822
v  TempK                    298.06          363.17          313.18          313.67
v  TurbVisc            8.5157e-023      0.00044953     4.2715e-006     1.5994e-005
v  CourantNb           5.0436e-005          1.2463         0.76905         0.97218
v  FourierNb             0.0029427               1         0.38201        0.083848
v  total_pressure      1.0082e+005     1.0152e+005     1.0134e+005     1.0136e+005
v  Local Time Step          1e-006       0.0072226     9.6028e-005      0.00026048

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.49          305.47
v  Yplus               0          2.9422         0.55772         0.40159


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46244               2          1.1511           1.056


 INSTANT    0.132000000E-02   TIME STEP NUMBER             132
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924720E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24363E-01 0.46849E+01
   Friction velocity        uk    :  0.24363E-01 0.46809E+01
   Dimensionless distance   yplus :  0.17474E-01 0.29419E+01
   Friction thermal sca.    tstar : -0.26568E-04 0.72936E+02
   Rough dim-less th. sca.  tplus :  0.12379E-01 0.20840E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19677E+00      11   0.63322E-05   0.40514E+02 0.15487E+03 
c  Velocity[X]                                      0.19820E+02 
c  Velocity[Y]                                      0.35645E+01 
c  Velocity[Z]                                      0.17129E+02 
c  Pressure     0.36533E-04      22   0.86168E-03   0.44509E-01 0.61116E+02 
c  k            0.44132E-03      15   0.37643E-03   0.95085E-02 0.28537E+03 
c  omega        0.27924E+07       1   0.48633E-06   0.14573E+09 0.20322E+01 
c  TempK        0.72617E+04       8   0.36942E-05   0.79828E+03 0.22234E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.0463e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.871          19.115      -0.0026306      -0.0056842
v  Velocity[Y]             -16.261          14.449        0.051184        0.067523
v  Velocity[Z]             -25.553          12.238         -1.6757        -0.48923
v  ǁVelocityǁ         0.00049148          25.739           6.584          5.3414
v  Pressure                 -503.3          191.84          19.944          32.376
v  k                   1.0523e-014          6.9564        0.013583        0.015001
v  omega                     9.391     2.7324e+008     1.2901e+006           75832
v  TempK                    298.06          363.17          313.32          313.71
v  TurbVisc            9.1801e-022      0.00047103     4.3597e-006     1.6334e-005
v  CourantNb           5.9282e-005          1.2428         0.76918         0.97214
v  FourierNb             0.0029368               1         0.38217        0.084343
v  total_pressure      1.0082e+005     1.0152e+005     1.0134e+005     1.0136e+005
v  Local Time Step          1e-006       0.0072154     9.5831e-005      0.00025968

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           303.5          305.47
v  Yplus               0          2.9419         0.55811          0.4023


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58404               2          1.1513          1.0565


 INSTANT    0.133000000E-02   TIME STEP NUMBER             133
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924727E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25627E-01 0.46849E+01
   Friction velocity        uk    :  0.25627E-01 0.46809E+01
   Dimensionless distance   yplus :  0.18370E-01 0.29416E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.72772E+02
   Rough dim-less th. sca.  tplus :  0.13014E-01 0.20838E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19720E+00      11   0.64131E-05   0.40213E+02 0.15359E+03 
c  Velocity[X]                                      0.19674E+02 
c  Velocity[Y]                                      0.35156E+01 
c  Velocity[Z]                                      0.17023E+02 
c  Pressure     0.36480E-04      22   0.86517E-03   0.44347E-01 0.58634E+02 
c  k            0.45214E-03      15   0.38382E-03   0.10055E-01 0.27672E+03 
c  omega        0.27924E+07       1   0.48461E-06   0.12690E+09 0.19067E+01 
c  TempK        0.72747E+04       8   0.36387E-05   0.78694E+03 0.22106E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.0704e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.837          19.089      -0.0025923      -0.0058378
v  Velocity[Y]              -16.15          14.405        0.051441        0.067855
v  Velocity[Z]             -25.549          12.714         -1.6762        -0.48896
v  ǁVelocityǁ         0.00048231          25.736          6.5939          5.3517
v  Pressure                -502.01           192.2          20.177          32.546
v  k                   9.8585e-014          6.8389        0.013842        0.015446
v  omega                    9.4991     2.7325e+008     1.2901e+006           75841
v  TempK                    298.06          363.17          313.46          313.74
v  TurbVisc            2.6556e-022      0.00046869     4.4508e-006     1.6683e-005
v  CourantNb           6.8984e-005          1.2391         0.76932         0.97211
v  FourierNb              0.002931               1         0.38233         0.08485
v  total_pressure      1.0082e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0072027     9.5638e-005      0.00025889

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           303.5          305.47
v  Yplus               0          2.9416          0.5585         0.40299


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56671               2          1.1516           1.057


 INSTANT    0.134000000E-02   TIME STEP NUMBER             134
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924722E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24955E-01 0.46851E+01
   Friction velocity        uk    :  0.24955E-01 0.46811E+01
   Dimensionless distance   yplus :  0.17889E-01 0.29413E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.72366E+02
   Rough dim-less th. sca.  tplus :  0.12673E-01 0.20837E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19764E+00      11   0.64841E-05   0.39910E+02 0.15230E+03 
c  Velocity[X]                                      0.19526E+02 
c  Velocity[Y]                                      0.34697E+01 
c  Velocity[Z]                                      0.16914E+02 
c  Pressure     0.36551E-04      21   0.86118E-03   0.44331E-01 0.58402E+02 
c  k            0.46349E-03      15   0.38794E-03   0.10629E-01 0.26912E+03 
c  omega        0.27924E+07       1   0.48362E-06   0.11722E+09 0.18333E+01 
c  TempK        0.72878E+04       8   0.35843E-05   0.77590E+03 0.21972E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.0952e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.815          19.063      -0.0025425      -0.0059828
v  Velocity[Y]             -16.093          14.375        0.051694        0.068175
v  Velocity[Z]             -25.546          13.298         -1.6769        -0.48871
v  ǁVelocityǁ         0.00030019          25.733          6.6039           5.362
v  Pressure                 -500.6          192.57          20.413           32.72
v  k                   2.4012e-013          6.7183        0.014105        0.015906
v  omega                    9.6084     2.7325e+008     1.2901e+006           75850
v  TempK                    298.07          363.17          313.59          313.78
v  TurbVisc             2.488e-021       0.0004931     4.5453e-006     1.7041e-005
v  CourantNb           6.7491e-005          1.2353         0.76945         0.97208
v  FourierNb             0.0029252               1          0.3825         0.08537
v  total_pressure      1.0082e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0070803     9.5447e-005      0.00025811

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.51          305.47
v  Yplus               0          2.9413         0.55889         0.40367


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47883               2           1.152          1.0575


 INSTANT    0.135000000E-02   TIME STEP NUMBER             135
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924639E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20297E-01 0.46853E+01
   Friction velocity        uk    :  0.20297E-01 0.46813E+01
   Dimensionless distance   yplus :  0.14533E-01 0.29411E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.71819E+02
   Rough dim-less th. sca.  tplus :  0.10295E-01 0.20835E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19807E+00      11   0.65826E-05   0.39619E+02 0.15104E+03 
c  Velocity[X]                                      0.19379E+02 
c  Velocity[Y]                                      0.34273E+01 
c  Velocity[Z]                                      0.16813E+02 
c  Pressure     0.36465E-04      20   0.86175E-03   0.44124E-01 0.56339E+02 
c  k            0.47536E-03      15   0.39093E-03   0.11226E-01 0.26258E+03 
c  omega        0.27924E+07       1   0.48303E-06   0.11479E+09 0.18041E+01 
c  TempK        0.73010E+04       8   0.35312E-05   0.76512E+03 0.21834E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.1206e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.796          19.038      -0.0024883      -0.0061152
v  Velocity[Y]              -16.09          14.368        0.051942        0.068481
v  Velocity[Z]             -25.544          13.925         -1.6775        -0.48844
v  ǁVelocityǁ         0.00043972           25.73          6.6137          5.3723
v  Pressure                -499.12          192.91          20.634          32.878
v  k                   4.4707e-013          6.6005        0.014371        0.016381
v  omega                    9.7188     2.7325e+008     1.2901e+006           75859
v  TempK                    298.07          363.17          313.72          313.81
v  TurbVisc            6.0601e-021       0.0004821     4.6438e-006     1.7409e-005
v  CourantNb           6.2802e-005          1.2314         0.76959         0.97204
v  FourierNb             0.0029196               1         0.38267        0.085901
v  total_pressure      1.0083e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0070543     9.5252e-005      0.00025732

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.51          305.47
v  Yplus               0          2.9411         0.55928         0.40434


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50181               2          1.1523          1.0579


 INSTANT    0.136000000E-02   TIME STEP NUMBER             136
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924676E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22828E-01 0.46857E+01
   Friction velocity        uk    :  0.22828E-01 0.46817E+01
   Dimensionless distance   yplus :  0.15851E-01 0.29409E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.71123E+02
   Rough dim-less th. sca.  tplus :  0.11229E-01 0.20834E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19851E+00      11   0.66568E-05   0.39327E+02 0.14977E+03 
c  Velocity[X]                                      0.19227E+02 
c  Velocity[Y]                                      0.33830E+01 
c  Velocity[Z]                                      0.16717E+02 
c  Pressure     0.36436E-04      22   0.85484E-03   0.43991E-01 0.54519E+02 
c  k            0.48781E-03      15   0.39702E-03   0.11833E-01 0.25640E+03 
c  omega        0.27924E+07       1   0.48368E-06   0.12475E+09 0.18521E+01 
c  TempK        0.73142E+04       8   0.34798E-05   0.75459E+03 0.21690E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.1464e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.78          19.013      -0.0024246      -0.0062298
v  Velocity[Y]             -16.195          14.452        0.052185        0.068775
v  Velocity[Z]             -25.541           14.19         -1.6781        -0.48818
v  ǁVelocityǁ         0.00038351          25.728          6.6234          5.3826
v  Pressure                -497.57          193.24          20.835          33.015
v  k                   7.4363e-013          6.4867         0.01464         0.01687
v  omega                    9.8306     2.7326e+008     1.2901e+006           75868
v  TempK                    298.07          363.17          313.85          313.85
v  TurbVisc            1.1283e-020      0.00048396     4.7458e-006     1.7787e-005
v  CourantNb           4.3679e-005          1.2275         0.76972         0.97199
v  FourierNb             0.0029142               1         0.38285        0.086439
v  total_pressure      1.0083e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0069431      9.505e-005      0.00025653

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.52          305.47
v  Yplus               0          2.9409         0.55966           0.405


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48874               2          1.1526          1.0584


 INSTANT    0.137000000E-02   TIME STEP NUMBER             137
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924724E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22362E-01 0.46862E+01
   Friction velocity        uk    :  0.22362E-01 0.46822E+01
   Dimensionless distance   yplus :  0.14390E-01 0.29407E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.70355E+02
   Rough dim-less th. sca.  tplus :  0.10194E-01 0.20832E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19895E+00      11   0.67125E-05   0.39047E+02 0.14853E+03 
c  Velocity[X]                                      0.19085E+02 
c  Velocity[Y]                                      0.33427E+01 
c  Velocity[Z]                                      0.16619E+02 
c  Pressure     0.36452E-04      22   0.84490E-03   0.43911E-01 0.51588E+02 
c  k            0.50084E-03      15   0.40651E-03   0.12554E-01 0.25198E+03 
c  omega        0.27924E+07       1   0.48447E-06   0.14093E+09 0.19441E+01 
c  TempK        0.73275E+04       8   0.34301E-05   0.74433E+03 0.21543E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.1727e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.763          18.988      -0.0023578      -0.0063311
v  Velocity[Y]             -16.211          14.596        0.052427        0.069056
v  Velocity[Z]             -25.538          13.809         -1.6787        -0.48793
v  ǁVelocityǁ         0.00045053          25.725          6.6331           5.393
v  Pressure                -495.93          193.53          21.001          33.116
v  k                   8.7649e-013          6.3772        0.014913        0.017375
v  omega                    9.9437     2.7326e+008     1.2901e+006           75877
v  TempK                    298.07          363.17          313.98          313.89
v  TurbVisc            1.8767e-020      0.00048643     4.8514e-006     1.8173e-005
v  CourantNb           2.4974e-005          1.2236         0.76984         0.97193
v  FourierNb             0.0029088               1         0.38304        0.086985
v  total_pressure      1.0083e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0064868     9.4844e-005      0.00025574

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.52          305.48
v  Yplus               0          2.9407         0.56006         0.40564


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43052               2          1.1529          1.0589


 INSTANT    0.138000000E-02   TIME STEP NUMBER             138
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924709E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24379E-01 0.46868E+01
   Friction velocity        uk    :  0.24379E-01 0.46827E+01
   Dimensionless distance   yplus :  0.15688E-01 0.29405E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.69539E+02
   Rough dim-less th. sca.  tplus :  0.11113E-01 0.20831E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19940E+00      11   0.67916E-05   0.38767E+02 0.14730E+03 
c  Velocity[X]                                      0.18948E+02 
c  Velocity[Y]                                      0.33006E+01 
c  Velocity[Z]                                      0.16519E+02 
c  Pressure     0.36459E-04      21   0.83414E-03   0.43822E-01 0.49579E+02 
c  k            0.51444E-03      15   0.41803E-03   0.13336E-01 0.24838E+03 
c  omega        0.27924E+07       1   0.48282E-06   0.12067E+09 0.18159E+01 
c  TempK        0.73409E+04       8   0.33823E-05   0.73433E+03 0.21392E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.2001e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.746          18.963      -0.0022839      -0.0064267
v  Velocity[Y]             -16.092          14.453        0.052669        0.069338
v  Velocity[Z]             -25.536          14.375         -1.6793        -0.48767
v  ǁVelocityǁ         0.00052285          25.722          6.6427          5.4033
v  Pressure                -494.25          193.79           21.14           33.19
v  k                   5.2916e-013          6.2701         0.01519        0.017894
v  omega                    10.058     2.7326e+008     1.2901e+006           75886
v  TempK                    298.07          363.17           314.1          313.92
v  TurbVisc            2.2096e-020       0.0004993     4.9617e-006      1.857e-005
v  CourantNb           2.9234e-005          1.2195         0.76996         0.97188
v  FourierNb             0.0029037               1         0.38323        0.087547
v  total_pressure      1.0083e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0059411     9.4636e-005      0.00025496

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.53          305.48
v  Yplus               0          2.9405         0.56044         0.40628


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.449               2          1.1532          1.0594


 INSTANT    0.139000000E-02   TIME STEP NUMBER             139
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924631E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.27189E-01 0.46874E+01
   Friction velocity        uk    :  0.27189E-01 0.46834E+01
   Dimensionless distance   yplus :  0.18837E-01 0.29404E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.69378E+02
   Rough dim-less th. sca.  tplus :  0.13344E-01 0.20830E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.19984E+00      11   0.69033E-05   0.38481E+02 0.14606E+03 
c  Velocity[X]                                      0.18812E+02 
c  Velocity[Y]                                      0.32511E+01 
c  Velocity[Z]                                      0.16417E+02 
c  Pressure     0.36796E-04      22   0.83019E-03   0.44129E-01 0.48794E+02 
c  k            0.52861E-03      15   0.43056E-03   0.14075E-01 0.24349E+03 
c  omega        0.27924E+07       1   0.48205E-06   0.11664E+09 0.17812E+01 
c  TempK        0.73543E+04       8   0.33364E-05   0.72457E+03 0.21238E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.4517e-007                             1
a  omega          
a  TempK          
a  Local Time Step     8.2276e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.729          18.938      -0.0022131      -0.0065279
v  Velocity[Y]             -16.021          14.412        0.052914        0.069628
v  Velocity[Z]             -25.533          14.834         -1.6799        -0.48742
v  ǁVelocityǁ         0.00051686           25.72          6.6522          5.4137
v  Pressure                -492.49          194.04          21.277          33.262
v  k                   1.4869e-013          6.1524        0.015472        0.018429
v  omega                    10.175     2.7327e+008     1.2901e+006           75895
v  TempK                    298.07          363.17          314.23          313.96
v  TurbVisc             1.334e-020      0.00051557     5.0761e-006     1.8974e-005
v  CourantNb           4.3239e-005          1.2154         0.77008         0.97181
v  FourierNb             0.0028988               1         0.38342         0.08812
v  total_pressure      1.0083e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0058027     9.4427e-005      0.00025419

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.54          305.48
v  Yplus               0          2.9404         0.56084         0.40692


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41855               2          1.1535          1.0599


 INSTANT    0.140000000E-02   TIME STEP NUMBER             140
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924634E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.26954E-01 0.46881E+01
   Friction velocity        uk    :  0.26954E-01 0.46841E+01
   Dimensionless distance   yplus :  0.19341E-01 0.29402E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.70164E+02
   Rough dim-less th. sca.  tplus :  0.13701E-01 0.20829E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20028E+00      11   0.69666E-05   0.38196E+02 0.14483E+03 
c  Velocity[X]                                      0.18674E+02 
c  Velocity[Y]                                      0.32074E+01 
c  Velocity[Z]                                      0.16314E+02 
c  Pressure     0.36303E-04      21   0.86263E-03   0.43437E-01 0.47323E+02 
c  k            0.54333E-03      15   0.44226E-03   0.14781E-01 0.23819E+03 
c  omega        0.27924E+07       1   0.48109E-06   0.11018E+09 0.17287E+01 
c  TempK        0.73678E+04       8   0.32926E-05   0.71507E+03 0.21080E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.3934e-007                             4
a  omega          
a  TempK          
a  Local Time Step     8.2552e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.713          18.914      -0.0021483      -0.0066236
v  Velocity[Y]             -16.005          14.377        0.053159        0.069915
v  Velocity[Z]             -25.531          15.489         -1.6805        -0.48716
v  ǁVelocityǁ         0.00052548          25.718          6.6617          5.4241
v  Pressure                 -490.7          194.27          21.394          33.314
v  k                   3.0183e-013          5.9976        0.015758        0.018979
v  omega                    10.292     2.7327e+008     1.2901e+006           75904
v  TempK                    298.08          363.17          314.35             314
v  TurbVisc            3.7484e-021      0.00051566     5.1935e-006     1.9385e-005
v  CourantNb           3.8893e-005          1.2114         0.77019         0.97174
v  FourierNb              0.002894               1         0.38362        0.088701
v  total_pressure      1.0083e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0056286     9.4219e-005      0.00025343

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.54          305.48
v  Yplus               0          2.9402         0.56124         0.40755


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50721               2          1.1538          1.0604


 INSTANT    0.141000000E-02   TIME STEP NUMBER             141
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924690E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.27089E-01 0.46888E+01
   Friction velocity        uk    :  0.27089E-01 0.46848E+01
   Dimensionless distance   yplus :  0.19438E-01 0.29401E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.70927E+02
   Rough dim-less th. sca.  tplus :  0.13770E-01 0.20828E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20073E+00      11   0.70636E-05   0.37908E+02 0.14359E+03 
c  Velocity[X]                                      0.18525E+02 
c  Velocity[Y]                                      0.31648E+01 
c  Velocity[Z]                                      0.16219E+02 
c  Pressure     0.36167E-04      23   0.83662E-03   0.43167E-01 0.46412E+02 
c  k            0.55857E-03      15   0.45135E-03   0.15506E-01 0.23336E+03 
c  omega        0.27924E+07       1   0.48097E-06   0.11349E+09 0.17386E+01 
c  TempK        0.73813E+04       8   0.32509E-05   0.70581E+03 0.20920E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.1421e-008                             7
a  omega          
a  TempK          
a  Local Time Step     8.2824e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.697           18.89      -0.0020906      -0.0067215
v  Velocity[Y]             -16.098          14.359        0.053399        0.070181
v  Velocity[Z]             -25.529          15.784         -1.6812        -0.48691
v  ǁVelocityǁ         0.00053666          25.716           6.671          5.4345
v  Pressure                -488.87          194.49          21.496           33.35
v  k                   7.5433e-013          5.8096        0.016047        0.019543
v  omega                    10.412     2.7327e+008     1.2901e+006           75913
v  TempK                    298.08          363.17          314.47          314.04
v  TurbVisc             7.609e-021      0.00050355     5.3145e-006     1.9802e-005
v  CourantNb           3.7566e-005          1.2074         0.77028         0.97165
v  FourierNb             0.0028894               1         0.38383        0.089283
v  total_pressure      1.0084e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0061679     9.4012e-005      0.00025267

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.55          305.48
v  Yplus               0          2.9401         0.56165         0.40818


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40722               2          1.1541          1.0609


 INSTANT    0.142000000E-02   TIME STEP NUMBER             142
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924951E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.27308E-01 0.46895E+01
   Friction velocity        uk    :  0.27308E-01 0.46855E+01
   Dimensionless distance   yplus :  0.19595E-01 0.29400E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.71627E+02
   Rough dim-less th. sca.  tplus :  0.13881E-01 0.20827E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20118E+00      11   0.71376E-05   0.37637E+02 0.14238E+03 
c  Velocity[X]                                      0.18382E+02 
c  Velocity[Y]                                      0.31296E+01 
c  Velocity[Z]                                      0.16125E+02 
c  Pressure     0.36282E-04      21   0.82688E-03   0.43195E-01 0.44921E+02 
c  k            0.57430E-03      15   0.45943E-03   0.16255E-01 0.22937E+03 
c  omega        0.27924E+07       1   0.48183E-06   0.13237E+09 0.18452E+01 
c  TempK        0.73949E+04       8   0.32114E-05   0.69680E+03 0.20756E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.1186e-008                             6
a  omega          
a  TempK          
a  Local Time Step     8.3092e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.681          18.866      -0.0020285      -0.0067913
v  Velocity[Y]             -16.106          14.402        0.053641        0.070431
v  Velocity[Z]             -25.527          16.312         -1.6818        -0.48666
v  ǁVelocityǁ         0.00056472          25.714          6.6803          5.4449
v  Pressure                -487.02          194.67          21.564          33.351
v  k                    6.564e-013            5.63        0.016341        0.020123
v  omega                    10.534     2.7328e+008     1.2902e+006           75922
v  TempK                    298.08          363.17          314.59          314.08
v  TurbVisc            1.9016e-020       0.0005101     5.4376e-006     2.0221e-005
v  CourantNb            3.657e-005          1.2035         0.77038         0.97156
v  FourierNb             0.0028849               1         0.38404        0.089863
v  total_pressure      1.0084e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0061608     9.3806e-005      0.00025192

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.55          305.48
v  Yplus               0            2.94         0.56205          0.4088


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38569               2          1.1544          1.0614


 INSTANT    0.143000000E-02   TIME STEP NUMBER             143
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924920E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.27993E-01 0.46901E+01
   Friction velocity        uk    :  0.27993E-01 0.46861E+01
   Dimensionless distance   yplus :  0.20087E-01 0.29398E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.72369E+02
   Rough dim-less th. sca.  tplus :  0.14230E-01 0.20826E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20163E+00      11   0.72112E-05   0.37368E+02 0.14117E+03 
c  Velocity[X]                                      0.18244E+02 
c  Velocity[Y]                                      0.30950E+01 
c  Velocity[Z]                                      0.16028E+02 
c  Pressure     0.36390E-04      21   0.81159E-03   0.43214E-01 0.44508E+02 
c  k            0.59056E-03      15   0.46418E-03   0.17009E-01 0.22549E+03 
c  omega        0.27924E+07       1   0.48042E-06   0.11744E+09 0.17507E+01 
c  TempK        0.74086E+04       8   0.31742E-05   0.68801E+03 0.20590E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -4.4239e-009                             6
a  omega          
a  TempK          
a  Local Time Step     8.3363e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.665          18.843      -0.0019784      -0.0068644
v  Velocity[Y]             -15.982           14.46        0.053885        0.070671
v  Velocity[Z]             -25.524          16.483         -1.6823        -0.48641
v  ǁVelocityǁ         0.00061406          25.712          6.6896          5.4553
v  Pressure                -485.15          194.85          21.643          33.365
v  k                   7.9884e-013          5.6182        0.016639        0.020715
v  omega                    10.657     2.7328e+008     1.2902e+006           75930
v  TempK                    298.09          363.17          314.71          314.12
v  TurbVisc            1.6548e-020      0.00050078     5.5635e-006     2.0645e-005
v  CourantNb           3.5776e-005          1.1996         0.77047         0.97146
v  FourierNb             0.0028805               1         0.38424        0.090444
v  total_pressure      1.0084e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0064491     9.3601e-005      0.00025119

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.56          305.48
v  Yplus               0          2.9398         0.56245          0.4094


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41336               2          1.1547          1.0619


 INSTANT    0.144000000E-02   TIME STEP NUMBER             144
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924694E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.29213E-01 0.46906E+01
   Friction velocity        uk    :  0.29213E-01 0.46866E+01
   Dimensionless distance   yplus :  0.18538E-01 0.29397E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.74183E+02
   Rough dim-less th. sca.  tplus :  0.13133E-01 0.20825E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20208E+00      11   0.73068E-05   0.37094E+02 0.13997E+03 
c  Velocity[X]                                      0.18103E+02 
c  Velocity[Y]                                      0.30571E+01 
c  Velocity[Z]                                      0.15934E+02 
c  Pressure     0.36345E-04      21   0.82042E-03   0.43054E-01 0.44153E+02 
c  k            0.60735E-03      15   0.46557E-03   0.17767E-01 0.22176E+03 
c  omega        0.27924E+07       1   0.47946E-06   0.11006E+09 0.17034E+01 
c  TempK        0.74223E+04       8   0.31392E-05   0.67939E+03 0.20422E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -1.5359e-009                             5
a  omega          
a  TempK          
a  Local Time Step     8.3625e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.65           18.82      -0.0019254      -0.0069317
v  Velocity[Y]             -15.905          14.416        0.054123        0.070894
v  Velocity[Z]             -25.522          16.963         -1.6829        -0.48617
v  ǁVelocityǁ         0.00056307           25.71          6.6987          5.4657
v  Pressure                -483.27          195.04           21.72          33.375
v  k                   7.9488e-013          5.6073         0.01694        0.021321
v  omega                    10.783     2.7329e+008     1.2902e+006           75939
v  TempK                    298.09          363.17          314.83          314.16
v  TurbVisc            2.0138e-020      0.00050315     5.6917e-006     2.1071e-005
v  CourantNb           3.5265e-005          1.1958         0.77055         0.97135
v  FourierNb             0.0028763               1         0.38445         0.09102
v  total_pressure      1.0084e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.007094     9.3395e-005      0.00025047

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.56          305.48
v  Yplus               0          2.9397         0.56285            0.41


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57087               2           1.155          1.0624


 INSTANT    0.145000000E-02   TIME STEP NUMBER             145
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924818E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25364E-01 0.46911E+01
   Friction velocity        uk    :  0.25364E-01 0.46870E+01
   Dimensionless distance   yplus :  0.14562E-01 0.29396E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.77758E+02
   Rough dim-less th. sca.  tplus :  0.10316E-01 0.20824E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20253E+00      11   0.73894E-05   0.36819E+02 0.13877E+03 
c  Velocity[X]                                      0.17961E+02 
c  Velocity[Y]                                      0.30161E+01 
c  Velocity[Z]                                      0.15842E+02 
c  Pressure     0.36346E-04      21   0.81946E-03   0.42949E-01 0.43059E+02 
c  k            0.62462E-03      15   0.46376E-03   0.18598E-01 0.21897E+03 
c  omega        0.27924E+07       1   0.47900E-06   0.11023E+09 0.17064E+01 
c  TempK        0.74361E+04       8   0.31063E-05   0.67096E+03 0.20251E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.372e-010                             4
a  omega          
a  TempK          
a  Local Time Step     8.3882e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.636          18.797      -0.0018772      -0.0070052
v  Velocity[Y]             -15.883          14.371        0.054356        0.071097
v  Velocity[Z]              -25.52          17.006         -1.6835        -0.48592
v  ǁVelocityǁ         0.00043647          25.708          6.7078          5.4762
v  Pressure                -481.38           195.2          21.767          33.355
v  k                   7.7123e-013          5.5973        0.017245        0.021938
v  omega                    10.911     2.7329e+008     1.2902e+006           75948
v  TempK                    298.09          363.17          314.94           314.2
v  TurbVisc            2.0039e-020      0.00049763     5.8213e-006     2.1497e-005
v  CourantNb           3.8226e-005          1.1921         0.77062         0.97124
v  FourierNb             0.0028722               1         0.38465        0.091584
v  total_pressure      1.0084e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0072539     9.3189e-005      0.00024976

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.57          305.48
v  Yplus               0          2.9396         0.56325          0.4106


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38154               2          1.1553          1.0628


 INSTANT    0.146000000E-02   TIME STEP NUMBER             146
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924889E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14974E-01 0.46914E+01
   Friction velocity        uk    :  0.14974E-01 0.46874E+01
   Dimensionless distance   yplus :  0.85972E-02 0.29395E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.81549E+02
   Rough dim-less th. sca.  tplus :  0.60903E-02 0.20824E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20298E+00      11   0.74678E-05   0.36553E+02 0.13760E+03 
c  Velocity[X]                                      0.17828E+02 
c  Velocity[Y]                                      0.29807E+01 
c  Velocity[Z]                                      0.15745E+02 
c  Pressure     0.36039E-04      21   0.81694E-03   0.42484E-01 0.42689E+02 
c  k            0.64240E-03      15   0.45947E-03   0.19500E-01 0.21721E+03 
c  omega        0.27924E+07       1   0.47865E-06   0.10991E+09 0.17068E+01 
c  TempK        0.74499E+04       8   0.30754E-05   0.66271E+03 0.20079E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                  -2.8628e-011                             2
a  omega          
a  TempK          
a  Local Time Step     8.4128e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.622          18.774      -0.0018275      -0.0070776
v  Velocity[Y]              -15.97          14.332        0.054581        0.071287
v  Velocity[Z]             -25.518          17.455          -1.684        -0.48567
v  ǁVelocityǁ         0.00038607          25.706          6.7169          5.4866
v  Pressure                -484.63          195.35          21.807          33.326
v  k                   6.1818e-013          5.5881        0.017553        0.022566
v  omega                    11.041     2.7329e+008     1.2902e+006           75957
v  TempK                     298.1          363.17          315.05          314.24
v  TurbVisc            1.9442e-020       0.0005015     5.9533e-006     2.1925e-005
v  CourantNb           4.0829e-005          1.1887         0.77069         0.97112
v  FourierNb             0.0028683               1         0.38484        0.092131
v  total_pressure      1.0084e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0077414     9.2979e-005      0.00024904

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.57          305.48
v  Yplus               0          2.9395         0.56366         0.41119


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38393               2          1.1555          1.0633


 INSTANT    0.147000000E-02   TIME STEP NUMBER             147
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925251E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16427E-01 0.46918E+01
   Friction velocity        uk    :  0.16427E-01 0.46878E+01
   Dimensionless distance   yplus :  0.94412E-02 0.29394E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.99246E+02
   Rough dim-less th. sca.  tplus :  0.66882E-02 0.20823E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20344E+00      11   0.75603E-05   0.36285E+02 0.13644E+03 
c  Velocity[X]                                      0.17686E+02 
c  Velocity[Y]                                      0.29485E+01 
c  Velocity[Z]                                      0.15651E+02 
c  Pressure     0.36008E-04      21   0.81976E-03   0.42346E-01 0.42203E+02 
c  k            0.66078E-03      15   0.45189E-03   0.20311E-01 0.21447E+03 
c  omega        0.27924E+07       1   0.47902E-06   0.12409E+09 0.18002E+01 
c  TempK        0.74639E+04       8   0.30467E-05   0.65466E+03 0.19904E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.897e-013                             1
a  omega          
a  TempK          
a  Local Time Step     8.4365e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.608          18.752      -0.0017787      -0.0071528
v  Velocity[Y]             -15.985          14.313        0.054802        0.071466
v  Velocity[Z]             -25.517          17.367         -1.6845        -0.48542
v  ǁVelocityǁ         0.00042794          25.704          6.7259           5.497
v  Pressure                -488.81          195.48          21.842          33.294
v  k                    1.897e-013          5.5795        0.017866        0.023203
v  omega                    11.174      2.733e+008     1.2902e+006           75965
v  TempK                     298.1          363.17          315.17          314.28
v  TurbVisc            1.5584e-020      0.00050519     6.0868e-006     2.2353e-005
v  CourantNb           4.1324e-005          1.1853         0.77076         0.97099
v  FourierNb             0.0028647               1         0.38502        0.092661
v  total_pressure      1.0084e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0085155     9.2771e-005      0.00024834

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.58          305.48
v  Yplus               0          2.9394         0.56408         0.41178


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46976               2          1.1558          1.0637


 INSTANT    0.148000000E-02   TIME STEP NUMBER             148
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924898E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20726E-01 0.46922E+01
   Friction velocity        uk    :  0.20726E-01 0.46881E+01
   Dimensionless distance   yplus :  0.11912E-01 0.29393E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.21719E+03
   Rough dim-less th. sca.  tplus :  0.84389E-02 0.20822E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20389E+00      11   0.76431E-05   0.36015E+02 0.13527E+03 
c  Velocity[X]                                      0.17540E+02 
c  Velocity[Y]                                      0.29135E+01 
c  Velocity[Z]                                      0.15562E+02 
c  Pressure     0.36003E-04      22   0.81528E-03   0.42242E-01 0.41907E+02 
c  k            0.67972E-03      15   0.44564E-03   0.21144E-01 0.21232E+03 
c  omega        0.27924E+07       1   0.47819E-06   0.11567E+09 0.17481E+01 
c  TempK        0.74778E+04       8   0.30200E-05   0.64677E+03 0.19727E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step       8.46e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.595           18.73      -0.0017326      -0.0072176
v  Velocity[Y]             -15.863          14.374        0.055023        0.071644
v  Velocity[Z]             -25.515          17.828          -1.685        -0.48516
v  ǁVelocityǁ         0.00053646          25.702          6.7349          5.5075
v  Pressure                -492.79          195.63          21.883          33.266
v  k                   8.2376e-013          5.5721        0.018184         0.02385
v  omega                    11.309      2.733e+008     1.2902e+006           75974
v  TempK                     298.1          363.17          315.28          314.33
v  TurbVisc            4.7823e-021       0.0005185     6.2212e-006      2.278e-005
v  CourantNb           4.1419e-005           1.182         0.77082         0.97087
v  FourierNb             0.0028612               1         0.38519        0.093175
v  total_pressure      1.0083e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0091852      9.256e-005      0.00024766

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.58          305.48
v  Yplus               0          2.9393         0.56449         0.41237


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4149               2           1.156           1.064


 INSTANT    0.149000000E-02   TIME STEP NUMBER             149
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925053E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.26353E-01 0.46926E+01
   Friction velocity        uk    :  0.26353E-01 0.46886E+01
   Dimensionless distance   yplus :  0.15146E-01 0.29392E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.11905E+03
   Rough dim-less th. sca.  tplus :  0.10730E-01 0.20822E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20435E+00      11   0.77480E-05   0.35751E+02 0.13411E+03 
c  Velocity[X]                                      0.17390E+02 
c  Velocity[Y]                                      0.28812E+01 
c  Velocity[Z]                                      0.15480E+02 
c  Pressure     0.36182E-04      22   0.81133E-03   0.42354E-01 0.41321E+02 
c  k            0.69926E-03      15   0.44092E-03   0.21973E-01 0.21069E+03 
c  omega        0.27924E+07       1   0.47711E-06   0.10928E+09 0.17108E+01 
c  TempK        0.74919E+04       8   0.29953E-05   0.63902E+03 0.19548E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.4823e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.582          18.708      -0.0016921         -0.0073
v  Velocity[Y]             -15.787          14.361        0.055242        0.071825
v  Velocity[Z]             -25.513          17.614         -1.6854        -0.48491
v  ǁVelocityǁ         0.00039835            25.7          6.7438           5.518
v  Pressure                -496.68          195.75          21.903          33.219
v  k                   2.0559e-012           5.566        0.018505        0.024504
v  omega                    11.448     2.7331e+008     1.2902e+006           75982
v  TempK                    298.11          363.17          315.39          314.37
v  TurbVisc            2.0767e-020      0.00052657     6.3557e-006     2.3202e-005
v  CourantNb           4.1668e-005          1.1789         0.77088         0.97074
v  FourierNb              0.002858               1         0.38535        0.093667
v  total_pressure      1.0083e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0091743      9.235e-005      0.00024698

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.59          305.48
v  Yplus               0          2.9392          0.5649         0.41294


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35267               2          1.1562          1.0644


 INSTANT    0.150000000E-02   TIME STEP NUMBER             150
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925139E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.30378E-01 0.46932E+01
   Friction velocity        uk    :  0.30378E-01 0.46891E+01
   Dimensionless distance   yplus :  0.17893E-01 0.29391E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.99040E+02
   Rough dim-less th. sca.  tplus :  0.12676E-01 0.20821E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20481E+00      11   0.78052E-05   0.35476E+02 0.13293E+03 
c  Velocity[X]                                      0.17240E+02 
c  Velocity[Y]                                      0.28478E+01 
c  Velocity[Z]                                      0.15388E+02 
c  Pressure     0.36153E-04      22   0.79442E-03   0.42224E-01 0.40987E+02 
c  k            0.71930E-03      15   0.43509E-03   0.22700E-01 0.20816E+03 
c  omega        0.27924E+07       1   0.47605E-06   0.10490E+09 0.16790E+01 
c  TempK        0.75059E+04       8   0.29723E-05   0.63142E+03 0.19368E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.5038e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.57          18.687      -0.0016483      -0.0073887
v  Velocity[Y]             -15.768          14.354         0.05546        0.072005
v  Velocity[Z]             -25.511           18.12         -1.6859        -0.48468
v  ǁVelocityǁ          0.0002415          25.699          6.7527          5.5284
v  Pressure                -500.38          195.87          21.918          33.165
v  k                   2.1394e-012          5.5614         0.01883        0.025166
v  omega                    11.589     2.7331e+008     1.2902e+006           75991
v  TempK                    298.11          363.17           315.5          314.41
v  TurbVisc            5.2057e-020      0.00054338     6.4911e-006     2.3622e-005
v  CourantNb           4.1837e-005          1.1759         0.77095         0.97064
v  FourierNb             0.0028551               1         0.38551        0.094149
v  total_pressure      1.0082e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0091275     9.2141e-005      0.00024631

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.59          305.48
v  Yplus               0          2.9391         0.56532         0.41351


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54986               2          1.1565          1.0648


 INSTANT    0.151000000E-02   TIME STEP NUMBER             151
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925242E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.29403E-01 0.46937E+01
   Friction velocity        uk    :  0.29403E-01 0.46897E+01
   Dimensionless distance   yplus :  0.19981E-01 0.29391E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.10391E+03
   Rough dim-less th. sca.  tplus :  0.14155E-01 0.20821E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20527E+00      11   0.78839E-05   0.35189E+02 0.13174E+03 
c  Velocity[X]                                      0.17082E+02 
c  Velocity[Y]                                      0.28139E+01 
c  Velocity[Z]                                      0.15293E+02 
c  Pressure     0.36260E-04      22   0.80251E-03   0.42258E-01 0.40680E+02 
c  k            0.73982E-03      15   0.43289E-03   0.23383E-01 0.20520E+03 
c  omega        0.27924E+07       1   0.47555E-06   0.11058E+09 0.17108E+01 
c  TempK        0.75201E+04       8   0.29512E-05   0.62398E+03 0.19186E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.5242e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.558          18.665      -0.0016081      -0.0074854
v  Velocity[Y]             -15.856          14.279        0.055665        0.072171
v  Velocity[Z]             -25.509          17.791         -1.6863        -0.48445
v  ǁVelocityǁ         0.00015157          25.697          6.7616          5.5389
v  Pressure                -503.89          195.98           21.93          33.107
v  k                    2.235e-012          5.5584        0.019157        0.025835
v  omega                    11.733     2.7331e+008     1.2902e+006           75999
v  TempK                    298.12          363.17           315.6          314.46
v  TurbVisc            5.4172e-020      0.00053804     6.6268e-006     2.4035e-005
v  CourantNb           4.2546e-005          1.1731         0.77103         0.97053
v  FourierNb             0.0028527               1         0.38566        0.094612
v  total_pressure      1.0082e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006         0.00908     9.1933e-005      0.00024564

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           303.6          305.49
v  Yplus               0          2.9391         0.56574         0.41408


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64836               2          1.1567          1.0651


 INSTANT    0.152000000E-02   TIME STEP NUMBER             152
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925366E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.31742E-01 0.46942E+01
   Friction velocity        uk    :  0.31742E-01 0.46902E+01
   Dimensionless distance   yplus :  0.21522E-01 0.29390E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.10778E+03
   Rough dim-less th. sca.  tplus :  0.15246E-01 0.20820E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20573E+00      11   0.79667E-05   0.34923E+02 0.13058E+03 
c  Velocity[X]                                      0.16933E+02 
c  Velocity[Y]                                      0.27847E+01 
c  Velocity[Z]                                      0.15205E+02 
c  Pressure     0.36000E-04      22   0.78006E-03   0.41864E-01 0.40220E+02 
c  k            0.76076E-03      15   0.43044E-03   0.24075E-01 0.20198E+03 
c  omega        0.27924E+07       1   0.47498E-06   0.11845E+09 0.17563E+01 
c  TempK        0.75342E+04       8   0.29318E-05   0.61668E+03 0.19002E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.5434e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.548          18.644      -0.0015718      -0.0075887
v  Velocity[Y]             -15.876          14.222        0.055862        0.072327
v  Velocity[Z]             -25.507          18.387         -1.6867        -0.48423
v  ǁVelocityǁ         0.00021276          25.695          6.7705          5.5495
v  Pressure                -507.21          196.07          21.925          33.033
v  k                   2.3445e-012          5.5573        0.019488        0.026509
v  omega                     11.88     2.7332e+008     1.2902e+006           76008
v  TempK                    298.13          363.17          315.71           314.5
v  TurbVisc            5.6593e-020      0.00054054      6.761e-006     2.4439e-005
v  CourantNb           4.3791e-005          1.1705         0.77111         0.97044
v  FourierNb             0.0028508               1          0.3858        0.095051
v  total_pressure      1.0082e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0090447     9.1729e-005        0.000245

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           303.6          305.49
v  Yplus               0           2.939         0.56616         0.41464


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48442               2          1.1569          1.0655


 INSTANT    0.153000000E-02   TIME STEP NUMBER             153
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925133E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.30983E-01 0.46947E+01
   Friction velocity        uk    :  0.30983E-01 0.46907E+01
   Dimensionless distance   yplus :  0.21007E-01 0.29390E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.11221E+03
   Rough dim-less th. sca.  tplus :  0.14881E-01 0.20820E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20619E+00      11   0.80686E-05   0.34657E+02 0.12944E+03 
c  Velocity[X]                                      0.16786E+02 
c  Velocity[Y]                                      0.27540E+01 
c  Velocity[Z]                                      0.15117E+02 
c  Pressure     0.35988E-04      21   0.77600E-03   0.41764E-01 0.39525E+02 
c  k            0.78208E-03      15   0.42900E-03   0.24930E-01 0.20064E+03 
c  omega        0.27924E+07       1   0.47275E-06   0.10225E+09 0.16501E+01 
c  TempK        0.75484E+04       8   0.29140E-05   0.60950E+03 0.18817E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.5627e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.538          18.623      -0.0015463      -0.0076916
v  Velocity[Y]              -15.76          14.189        0.056054        0.072484
v  Velocity[Z]             -25.506          17.968          -1.687        -0.48401
v  ǁVelocityǁ         0.00034455          25.694          6.7793            5.56
v  Pressure                 -510.3          196.17          21.937          32.976
v  k                   2.4696e-012          5.5582        0.019823        0.027187
v  omega                    12.029     2.7332e+008     1.2902e+006           76016
v  TempK                    298.13          363.17          315.81          314.55
v  TurbVisc            5.9364e-020      0.00055131     6.8933e-006     2.4831e-005
v  CourantNb           4.7501e-005          1.1679          0.7712         0.97037
v  FourierNb             0.0028496               1         0.38594        0.095466
v  total_pressure      1.0081e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0088066     9.1525e-005      0.00024436

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.61          305.49
v  Yplus               0           2.939         0.56659         0.41519


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44883               2          1.1571          1.0658


 INSTANT    0.154000000E-02   TIME STEP NUMBER             154
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925356E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.30269E-01 0.46952E+01
   Friction velocity        uk    :  0.30269E-01 0.46912E+01
   Dimensionless distance   yplus :  0.20523E-01 0.29389E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.11437E+03
   Rough dim-less th. sca.  tplus :  0.14538E-01 0.20820E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20665E+00      11   0.81449E-05   0.34399E+02 0.12831E+03 
c  Velocity[X]                                      0.16648E+02 
c  Velocity[Y]                                      0.27193E+01 
c  Velocity[Z]                                      0.15031E+02 
c  Pressure     0.36115E-04      21   0.77265E-03   0.41823E-01 0.39188E+02 
c  k            0.80374E-03      15   0.42541E-03   0.25913E-01 0.20041E+03 
c  omega        0.27924E+07       1   0.47168E-06   0.10223E+09 0.16448E+01 
c  TempK        0.75627E+04       8   0.28977E-05   0.60245E+03 0.18631E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.5807e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.529          18.603      -0.0015247       -0.007789
v  Velocity[Y]             -15.689          14.223        0.056239        0.072641
v  Velocity[Z]             -25.504           18.66         -1.6873        -0.48381
v  ǁVelocityǁ         0.00048714          25.693          6.7881          5.5706
v  Pressure                -512.92          196.26          21.934          32.902
v  k                   2.6124e-012          5.5613        0.020161        0.027871
v  omega                    12.182     2.7333e+008     1.2902e+006           76024
v  TempK                    298.14          363.17          315.92           314.6
v  TurbVisc            6.2532e-020      0.00056638     7.0225e-006      2.521e-005
v  CourantNb           5.1057e-005          1.1654          0.7713         0.97031
v  FourierNb             0.0028491               1         0.38606        0.095848
v  total_pressure      1.0081e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0084197     9.1321e-005      0.00024373

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.61          305.49
v  Yplus               0          2.9389         0.56701         0.41574


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42004               2          1.1574          1.0662


 INSTANT    0.155000000E-02   TIME STEP NUMBER             155
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925266E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.29589E-01 0.46957E+01
   Friction velocity        uk    :  0.29589E-01 0.46917E+01
   Dimensionless distance   yplus :  0.18566E-01 0.29389E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.11640E+03
   Rough dim-less th. sca.  tplus :  0.13152E-01 0.20819E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20711E+00      11   0.82084E-05   0.34145E+02 0.12723E+03 
c  Velocity[X]                                      0.16514E+02 
c  Velocity[Y]                                      0.26890E+01 
c  Velocity[Z]                                      0.14942E+02 
c  Pressure     0.35873E-04      22   0.76751E-03   0.41463E-01 0.38826E+02 
c  k            0.82574E-03      15   0.41934E-03   0.26995E-01 0.20062E+03 
c  omega        0.27924E+07       1   0.47040E-06   0.10146E+09 0.16344E+01 
c  TempK        0.75770E+04       8   0.28830E-05   0.59551E+03 0.18444E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.5979e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.52          18.582      -0.0015083      -0.0078751
v  Velocity[Y]             -15.673          14.272        0.056413        0.072789
v  Velocity[Z]             -25.503          18.244         -1.6876        -0.48362
v  ǁVelocityǁ         0.00047459          25.691          6.7969          5.5812
v  Pressure                -515.19          196.34           21.93          32.826
v  k                   2.7754e-012          5.5665        0.020503        0.028558
v  omega                    12.339     2.7333e+008     1.2902e+006           76032
v  TempK                    298.15          363.17          316.02          314.65
v  TurbVisc            6.6149e-020      0.00060243     7.1505e-006      2.558e-005
v  CourantNb           5.4474e-005          1.1631         0.77141         0.97027
v  FourierNb             0.0028492               1         0.38617        0.096207
v  total_pressure      1.0081e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0089824     9.1116e-005       0.0002431

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.61          305.49
v  Yplus               0          2.9389         0.56744         0.41628


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52992               2          1.1576          1.0665


 INSTANT    0.156000000E-02   TIME STEP NUMBER             156
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925263E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14045E-01 0.46961E+01
   Friction velocity        uk    :  0.14045E-01 0.46921E+01
   Dimensionless distance   yplus :  0.96228E-02 0.29388E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.11530E+03
   Rough dim-less th. sca.  tplus :  0.68169E-02 0.20819E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20757E+00      11   0.82702E-05   0.33893E+02 0.12616E+03 
c  Velocity[X]                                      0.16383E+02 
c  Velocity[Y]                                      0.26617E+01 
c  Velocity[Z]                                      0.14848E+02 
c  Pressure     0.35789E-04      23   0.76309E-03   0.41287E-01 0.38439E+02 
c  k            0.84806E-03      15   0.41266E-03   0.28135E-01 0.20125E+03 
c  omega        0.27924E+07       1   0.46916E-06   0.10073E+09 0.16243E+01 
c  TempK        0.75913E+04       8   0.28696E-05   0.58868E+03 0.18255E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.6138e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.513          18.561      -0.0014949      -0.0079522
v  Velocity[Y]             -15.762          14.224        0.056569        0.072926
v  Velocity[Z]             -25.501            18.8         -1.6879        -0.48345
v  ǁVelocityǁ         0.00055027           25.69          6.8057          5.5919
v  Pressure                -517.12          196.42          21.924          32.748
v  k                   2.8589e-012          5.5738        0.020851        0.029248
v  omega                    12.498     2.7333e+008     1.2902e+006           76041
v  TempK                    298.15          363.17          316.12           314.7
v  TurbVisc            7.0274e-020      0.00060495     7.2764e-006      2.594e-005
v  CourantNb           5.7475e-005          1.1609         0.77154         0.97024
v  FourierNb             0.0028501               1         0.38628        0.096537
v  total_pressure      1.0081e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0089041     9.0911e-005      0.00024247

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.62          305.49
v  Yplus               0          2.9388         0.56786         0.41682


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48184               2          1.1578          1.0668


 INSTANT    0.157000000E-02   TIME STEP NUMBER             157
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925313E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23103E-01 0.46965E+01
   Friction velocity        uk    :  0.23103E-01 0.46925E+01
   Dimensionless distance   yplus :  0.13259E-01 0.29388E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.11366E+03
   Rough dim-less th. sca.  tplus :  0.93924E-02 0.20818E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20804E+00      11   0.83548E-05   0.33647E+02 0.12510E+03 
c  Velocity[X]                                      0.16257E+02 
c  Velocity[Y]                                      0.26326E+01 
c  Velocity[Z]                                      0.14757E+02 
c  Pressure     0.35897E-04      24   0.75791E-03   0.41336E-01 0.38092E+02 
c  k            0.87064E-03      15   0.40250E-03   0.29285E-01 0.20213E+03 
c  omega        0.27924E+07       1   0.46862E-06   0.11472E+09 0.17083E+01 
c  TempK        0.76057E+04       8   0.28576E-05   0.58198E+03 0.18066E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.6287e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.506          18.541      -0.0014854      -0.0080247
v  Velocity[Y]             -15.785          14.174        0.056713        0.073056
v  Velocity[Z]               -25.5          18.612         -1.6881        -0.48328
v  ǁVelocityǁ         0.00065977          25.688          6.8144          5.6025
v  Pressure                -518.72           196.5          21.918          32.668
v  k                   2.9529e-012          5.5887        0.021203        0.029942
v  omega                     12.66     2.7334e+008     1.2902e+006           76049
v  TempK                    298.15          363.17          316.22          314.75
v  TurbVisc            7.2435e-020      0.00060412     7.3989e-006     2.6286e-005
v  CourantNb           5.9135e-005          1.1589         0.77167         0.97023
v  FourierNb             0.0028516               1         0.38637        0.096836
v  total_pressure      1.0081e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0092122     9.0708e-005      0.00024186

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.62          305.49
v  Yplus               0          2.9388         0.56829         0.41735


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39466               2           1.158          1.0671


 INSTANT    0.158000000E-02   TIME STEP NUMBER             158
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924936E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.27856E-01 0.46969E+01
   Friction velocity        uk    :  0.27855E-01 0.46929E+01
   Dimensionless distance   yplus :  0.17161E-01 0.29387E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.10948E+03
   Rough dim-less th. sca.  tplus :  0.12157E-01 0.20818E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20850E+00      11   0.84136E-05   0.33402E+02 0.12404E+03 
c  Velocity[X]                                      0.16126E+02 
c  Velocity[Y]                                      0.26046E+01 
c  Velocity[Z]                                      0.14671E+02 
c  Pressure     0.35957E-04      22   0.75570E-03   0.41328E-01 0.37569E+02 
c  k            0.89344E-03      15   0.39300E-03   0.30264E-01 0.20173E+03 
c  omega        0.27924E+07       1   0.46611E-06   0.97170E+08 0.15804E+01 
c  TempK        0.76201E+04       8   0.28466E-05   0.57536E+03 0.17875E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.6437e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -18.5           18.52      -0.0014844      -0.0081011
v  Velocity[Y]             -15.666          14.133        0.056848        0.073189
v  Velocity[Z]             -25.499          18.846         -1.6883        -0.48311
v  ǁVelocityǁ         0.00053014          25.687          6.8232          5.6132
v  Pressure                 -520.1          196.59          21.922            32.6
v  k                    3.059e-012          5.6163        0.021559        0.030637
v  omega                    12.826     2.7334e+008     1.2902e+006           76057
v  TempK                    298.15          363.17          316.32           314.8
v  TurbVisc            7.4816e-020      0.00061249     7.5171e-006     2.6616e-005
v  CourantNb           6.0917e-005          1.1569         0.77182         0.97025
v  FourierNb             0.0028539               1         0.38644        0.097103
v  total_pressure       1.008e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0094522     9.0507e-005      0.00024126

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.63          305.49
v  Yplus               0          2.9387         0.56871         0.41786


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.27969               2          1.1583          1.0674


 INSTANT    0.159000000E-02   TIME STEP NUMBER             159
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925173E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25587E-01 0.46973E+01
   Friction velocity        uk    :  0.25587E-01 0.46932E+01
   Dimensionless distance   yplus :  0.14701E-01 0.29387E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.10597E+03
   Rough dim-less th. sca.  tplus :  0.10415E-01 0.20818E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20896E+00      11   0.84605E-05   0.33136E+02 0.12296E+03 
c  Velocity[X]                                      0.15977E+02 
c  Velocity[Y]                                      0.25731E+01 
c  Velocity[Z]                                      0.14586E+02 
c  Pressure     0.35819E-04      22   0.74274E-03   0.41094E-01 0.37135E+02 
c  k            0.91643E-03      15   0.38188E-03   0.31016E-01 0.19970E+03 
c  omega        0.27924E+07       1   0.46435E-06   0.90885E+08 0.15256E+01 
c  TempK        0.76346E+04       8   0.28368E-05   0.56884E+03 0.17683E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.6575e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.494            18.5      -0.0014836      -0.0081928
v  Velocity[Y]              -15.59          14.114        0.056973        0.073325
v  Velocity[Z]             -25.502          18.783         -1.6884        -0.48295
v  ǁVelocityǁ         0.00035514          25.686          6.8319           5.624
v  Pressure                -521.18          196.66          21.923          32.527
v  k                   3.1787e-012          5.6458        0.021918        0.031335
v  omega                    12.994     2.7334e+008     1.2902e+006           76065
v  TempK                    298.15          363.17          316.42          314.85
v  TurbVisc            7.7506e-020      0.00062842     7.6325e-006     2.6934e-005
v  CourantNb           6.3538e-005          1.1551         0.77198          0.9703
v  FourierNb             0.0028571               1          0.3865        0.097339
v  total_pressure       1.008e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0094816     9.0302e-005      0.00024066

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.63          305.49
v  Yplus               0          2.9387         0.56912         0.41837


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42785               2          1.1585          1.0676


 INSTANT    0.160000000E-02   TIME STEP NUMBER             160
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925014E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21731E-01 0.46976E+01
   Friction velocity        uk    :  0.21731E-01 0.46936E+01
   Dimensionless distance   yplus :  0.12486E-01 0.29386E+01
   Friction thermal sca.    tstar :  0.00000E+00 0.10114E+03
   Rough dim-less th. sca.  tplus :  0.88450E-02 0.20817E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20943E+00      11   0.85011E-05   0.32865E+02 0.12188E+03 
c  Velocity[X]                                      0.15828E+02 
c  Velocity[Y]                                      0.25448E+01 
c  Velocity[Z]                                      0.14492E+02 
c  Pressure     0.35436E-04      22   0.74586E-03   0.40581E-01 0.36821E+02 
c  k            0.93959E-03      15   0.37304E-03   0.31504E-01 0.19609E+03 
c  omega        0.27924E+07       1   0.46338E-06   0.94782E+08 0.15428E+01 
c  TempK        0.76491E+04       8   0.28280E-05   0.56241E+03 0.17491E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.6705e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.49          18.479      -0.0014823      -0.0082848
v  Velocity[Y]              -15.57          14.178        0.057092        0.073461
v  Velocity[Z]             -25.504          18.842         -1.6886         -0.4828
v  ǁVelocityǁ         0.00022821          25.685          6.8407          5.6347
v  Pressure                -521.91          196.75          21.933          32.464
v  k                   3.3132e-012          5.6771        0.022281        0.032034
v  omega                    13.167     2.7335e+008     1.2902e+006           76072
v  TempK                    298.15          363.17          316.52          314.91
v  TurbVisc            8.0538e-020      0.00063769     7.7447e-006     2.7239e-005
v  CourantNb           6.6166e-005          1.1533         0.77216         0.97035
v  FourierNb             0.0028609               1         0.38654         0.09754
v  total_pressure       1.008e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0095045     9.0098e-005      0.00024006

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.63          305.49
v  Yplus               0          2.9386         0.56953         0.41887


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44965               2          1.1587          1.0679


 INSTANT    0.161000000E-02   TIME STEP NUMBER             161
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925110E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17756E-01 0.46979E+01
   Friction velocity        uk    :  0.17756E-01 0.46939E+01
   Dimensionless distance   yplus :  0.11372E-01 0.29385E+01
   Friction thermal sca.    tstar :  0.25098E-12 0.96930E+02
   Rough dim-less th. sca.  tplus :  0.80562E-02 0.20817E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.20989E+00      11   0.85611E-05   0.32616E+02 0.12085E+03 
c  Velocity[X]                                      0.15682E+02 
c  Velocity[Y]                                      0.25229E+01 
c  Velocity[Z]                                      0.14411E+02 
c  Pressure     0.35164E-04      22   0.74869E-03   0.40201E-01 0.36449E+02 
c  k            0.96286E-03      15   0.36451E-03   0.32027E-01 0.19313E+03 
c  omega        0.27924E+07       1   0.46208E-06   0.95268E+08 0.15383E+01 
c  TempK        0.76637E+04       8   0.28202E-05   0.55605E+03 0.17298E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.6824e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.487          18.459      -0.0014793       -0.008365
v  Velocity[Y]             -15.655          14.173        0.057198        0.073593
v  Velocity[Z]             -25.505          18.782         -1.6887        -0.48266
v  ǁVelocityǁ         0.00049824          25.683          6.8494          5.6455
v  Pressure                 -522.3          196.84          21.944            32.4
v  k                   3.4642e-012          5.7104        0.022646        0.032735
v  omega                    13.342     2.7335e+008     1.2902e+006           76080
v  TempK                    298.15          363.17          316.62          314.96
v  TurbVisc            8.3947e-020      0.00064026     7.8538e-006     2.7533e-005
v  CourantNb           6.8751e-005          1.1517         0.77235         0.97043
v  FourierNb             0.0028656               1         0.38657        0.097706
v  total_pressure       1.008e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0095174     8.9891e-005      0.00023945

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.64          305.49
v  Yplus               0          2.9385         0.56995         0.41937


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45582               2          1.1589          1.0681


 INSTANT    0.162000000E-02   TIME STEP NUMBER             162
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925155E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21704E-01 0.46981E+01
   Friction velocity        uk    :  0.21704E-01 0.46941E+01
   Dimensionless distance   yplus :  0.12471E-01 0.29384E+01
   Friction thermal sca.    tstar :  0.25060E-12 0.97368E+02
   Rough dim-less th. sca.  tplus :  0.88342E-02 0.20816E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21036E+00      11   0.86094E-05   0.32358E+02 0.11981E+03 
c  Velocity[X]                                      0.15526E+02 
c  Velocity[Y]                                      0.25015E+01 
c  Velocity[Z]                                      0.14331E+02 
c  Pressure     0.34866E-04      21   0.73385E-03   0.39797E-01 0.35967E+02 
c  k            0.98629E-03      15   0.35678E-03   0.32741E-01 0.19217E+03 
c  omega        0.27924E+07       1   0.46117E-06   0.10606E+09 0.16084E+01 
c  TempK        0.76783E+04       8   0.28133E-05   0.54980E+03 0.17104E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.6934e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.484          18.438      -0.0014686      -0.0084481
v  Velocity[Y]             -15.676          14.171        0.057297        0.073722
v  Velocity[Z]             -25.505          18.734         -1.6887        -0.48251
v  ǁVelocityǁ         0.00057715          25.682          6.8581          5.6562
v  Pressure                -522.36          196.93           21.96          32.341
v  k                   3.6331e-012          5.7455        0.023013        0.033436
v  omega                    13.521     2.7335e+008     1.2903e+006           76088
v  TempK                    298.15          363.17          316.71          315.02
v  TurbVisc            8.7771e-020      0.00065254     7.9591e-006     2.7816e-005
v  CourantNb            7.131e-005          1.1503         0.77254         0.97052
v  FourierNb             0.0028713               1         0.38658        0.097833
v  total_pressure       1.008e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.009512     8.9682e-005      0.00023882

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.64           305.5
v  Yplus               0          2.9384         0.57036         0.41986


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62425               2          1.1591          1.0683


 INSTANT    0.163000000E-02   TIME STEP NUMBER             163
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925019E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25509E-01 0.46983E+01
   Friction velocity        uk    :  0.25509E-01 0.46943E+01
   Dimensionless distance   yplus :  0.14656E-01 0.29383E+01
   Friction thermal sca.    tstar :  0.29512E-12 0.98218E+02
   Rough dim-less th. sca.  tplus :  0.10383E-01 0.20815E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21082E+00      11   0.86214E-05   0.32103E+02 0.11879E+03 
c  Velocity[X]                                      0.15376E+02 
c  Velocity[Y]                                      0.24815E+01 
c  Velocity[Z]                                      0.14246E+02 
c  Pressure     0.34938E-04      21   0.72236E-03   0.39822E-01 0.35562E+02 
c  k            0.10100E-02      15   0.34862E-03   0.33647E-01 0.19288E+03 
c  omega        0.27924E+07       1   0.45866E-06   0.95302E+08 0.15284E+01 
c  TempK        0.76930E+04       8   0.28072E-05   0.54362E+03 0.16910E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7047e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.481          18.418      -0.0014611      -0.0085138
v  Velocity[Y]             -15.557          14.104        0.057385         0.07384
v  Velocity[Z]             -25.505          18.682         -1.6888        -0.48237
v  ǁVelocityǁ         0.00046011          25.681          6.8668           5.667
v  Pressure                 -522.1          197.03          21.989          32.296
v  k                   3.8218e-012          5.7829        0.023384        0.034138
v  omega                    13.704     2.7336e+008     1.2903e+006           76095
v  TempK                    298.15          363.17          316.81          315.07
v  TurbVisc            9.2052e-020      0.00066451     8.0623e-006     2.8091e-005
v  CourantNb           7.4479e-005          1.1488         0.77274         0.97061
v  FourierNb             0.0028783               1         0.38658        0.097929
v  total_pressure       1.008e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0078988     8.9469e-005       0.0002382

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.65           305.5
v  Yplus               0          2.9383         0.57077         0.42034


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.37826               2          1.1593          1.0685


 INSTANT    0.164000000E-02   TIME STEP NUMBER             164
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924461E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25382E-01 0.46985E+01
   Friction velocity        uk    :  0.25382E-01 0.46945E+01
   Dimensionless distance   yplus :  0.16802E-01 0.29383E+01
   Friction thermal sca.    tstar :  0.49977E-12 0.98856E+02
   Rough dim-less th. sca.  tplus :  0.11903E-01 0.20815E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21128E+00      11   0.86552E-05   0.31849E+02 0.11778E+03 
c  Velocity[X]                                      0.15232E+02 
c  Velocity[Y]                                      0.24580E+01 
c  Velocity[Z]                                      0.14159E+02 
c  Pressure     0.34639E-04      21   0.71331E-03   0.39424E-01 0.36115E+02 
c  k            0.10339E-02      15   0.34280E-03   0.34664E-01 0.19448E+03 
c  omega        0.27924E+07       1   0.45630E-06   0.84925E+08 0.14458E+01 
c  TempK        0.77076E+04       8   0.28016E-05   0.53752E+03 0.16715E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7149e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.477          18.397       -0.001447      -0.0085739
v  Velocity[Y]             -15.477          14.054        0.057459        0.073953
v  Velocity[Z]             -25.505          18.603         -1.6887        -0.48223
v  ǁVelocityǁ         0.00072357           25.68          6.8755          5.6778
v  Pressure                -521.57          197.17          22.055          32.287
v  k                   4.0321e-012          5.8226        0.023759        0.034842
v  omega                    13.891     2.7336e+008     1.2903e+006           76103
v  TempK                    298.15          363.17           316.9          315.13
v  TurbVisc            9.6833e-020      0.00067527     8.1626e-006     2.8356e-005
v  CourantNb            7.149e-005          1.1475         0.77295         0.97072
v  FourierNb             0.0028867               1         0.38656         0.09799
v  total_pressure       1.008e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0071215     8.9252e-005      0.00023758

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.65           305.5
v  Yplus               0          2.9383         0.57118         0.42082


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68841               2          1.1595          1.0687


 INSTANT    0.165000000E-02   TIME STEP NUMBER             165
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924410E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25767E-01 0.46987E+01
   Friction velocity        uk    :  0.25767E-01 0.46947E+01
   Dimensionless distance   yplus :  0.17471E-01 0.29382E+01
   Friction thermal sca.    tstar :  0.74861E-12 0.99469E+02
   Rough dim-less th. sca.  tplus :  0.12376E-01 0.20814E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21175E+00      11   0.86640E-05   0.31594E+02 0.11681E+03 
c  Velocity[X]                                      0.15090E+02 
c  Velocity[Y]                                      0.24390E+01 
c  Velocity[Z]                                      0.14065E+02 
c  Pressure     0.34360E-04      21   0.70682E-03   0.39052E-01 0.36233E+02 
c  k            0.10581E-02      15   0.33443E-03   0.35690E-01 0.19594E+03 
c  omega        0.27924E+07       1   0.45470E-06   0.83879E+08 0.14348E+01 
c  TempK        0.77223E+04       8   0.27967E-05   0.53151E+03 0.16521E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7245e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.473          18.377      -0.0014369      -0.0086452
v  Velocity[Y]             -15.454          14.028        0.057525        0.074066
v  Velocity[Z]             -25.504          18.569         -1.6887         -0.4821
v  ǁVelocityǁ         0.00036233          25.679          6.8842          5.6885
v  Pressure                -520.79          197.32          22.131          32.289
v  k                   4.2657e-012          5.8649        0.024139        0.035545
v  omega                    14.081     2.7336e+008     1.2903e+006           76110
v  TempK                    298.15          363.17             317          315.19
v  TurbVisc            1.0216e-019      0.00067328     8.2607e-006     2.8613e-005
v  CourantNb           6.7486e-005          1.1462         0.77316         0.97083
v  FourierNb             0.0028847               1         0.38652        0.098013
v  total_pressure       1.008e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0068104     8.9026e-005      0.00023694

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.65           305.5
v  Yplus               0          2.9382         0.57159          0.4213


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5986               2          1.1597          1.0688


 INSTANT    0.166000000E-02   TIME STEP NUMBER             166
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924315E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22363E-01 0.46989E+01
   Friction velocity        uk    :  0.22363E-01 0.46949E+01
   Dimensionless distance   yplus :  0.16047E-01 0.29381E+01
   Friction thermal sca.    tstar :  0.10768E-11 0.10125E+03
   Rough dim-less th. sca.  tplus :  0.11368E-01 0.20814E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21221E+00      11   0.86346E-05   0.31349E+02 0.11587E+03 
c  Velocity[X]                                      0.14953E+02 
c  Velocity[Y]                                      0.24188E+01 
c  Velocity[Z]                                      0.13977E+02 
c  Pressure     0.34090E-04      22   0.70288E-03   0.38690E-01 0.36409E+02 
c  k            0.10826E-02      15   0.32930E-03   0.36644E-01 0.19688E+03 
c  omega        0.27924E+07       1   0.45373E-06   0.89364E+08 0.14680E+01 
c  TempK        0.77370E+04       8   0.27925E-05   0.52559E+03 0.16325E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7329e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.469          18.357      -0.0014275       -0.008703
v  Velocity[Y]             -15.515           14.04        0.057582        0.074179
v  Velocity[Z]             -25.503          18.495         -1.6886        -0.48198
v  ǁVelocityǁ         0.00050615          25.678          6.8929          5.6993
v  Pressure                -519.81          197.48          22.215          32.299
v  k                   4.4026e-012          5.9099        0.024523         0.03625
v  omega                    14.275     2.7336e+008     1.2903e+006           76118
v  TempK                    298.15          363.17          317.09          315.25
v  TurbVisc            1.0808e-019      0.00066321     8.3564e-006     2.8861e-005
v  CourantNb           6.3121e-005          1.1451         0.77337         0.97094
v  FourierNb             0.0028798               1         0.38647        0.098003
v  total_pressure      1.0081e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0067786     8.8799e-005       0.0002363

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.66           305.5
v  Yplus               0          2.9381           0.572         0.42177


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51119               2          1.1598          1.0689


 INSTANT    0.167000000E-02   TIME STEP NUMBER             167
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924252E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25679E-01 0.46990E+01
   Friction velocity        uk    :  0.25679E-01 0.46950E+01
   Dimensionless distance   yplus :  0.17411E-01 0.29380E+01
   Friction thermal sca.    tstar :  0.14557E-11 0.10297E+03
   Rough dim-less th. sca.  tplus :  0.12334E-01 0.20813E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21267E+00      11   0.86157E-05   0.31107E+02 0.11495E+03 
c  Velocity[X]                                      0.14819E+02 
c  Velocity[Y]                                      0.24034E+01 
c  Velocity[Z]                                      0.13885E+02 
c  Pressure     0.33835E-04      21   0.69495E-03   0.38349E-01 0.35902E+02 
c  k            0.11074E-02      15   0.32262E-03   0.37444E-01 0.19697E+03 
c  omega        0.27924E+07       1   0.45304E-06   0.97377E+08 0.15230E+01 
c  TempK        0.77517E+04       8   0.27889E-05   0.51973E+03 0.16130E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7403e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.464          18.338      -0.0014121      -0.0087467
v  Velocity[Y]             -15.546          14.145        0.057633        0.074292
v  Velocity[Z]             -25.501          18.502         -1.6885        -0.48186
v  ǁVelocityǁ          0.0008165          25.676          6.9016            5.71
v  Pressure                -518.68          197.63          22.293          32.302
v  k                   4.4133e-012          5.9576        0.024912        0.036955
v  omega                    14.474     2.7337e+008     1.2903e+006           76125
v  TempK                    298.15          363.17          317.18          315.31
v  TurbVisc            1.1109e-019      0.00064778       8.45e-006     2.9104e-005
v  CourantNb           5.8636e-005          1.1441         0.77358         0.97106
v  FourierNb             0.0028763               1         0.38641        0.097962
v  total_pressure      1.0081e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0067917     8.8569e-005      0.00023566

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.66           305.5
v  Yplus               0           2.938         0.57242         0.42224


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44925               2            1.16           1.069


 INSTANT    0.168000000E-02   TIME STEP NUMBER             168
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924361E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25677E-01 0.46992E+01
   Friction velocity        uk    :  0.25677E-01 0.46952E+01
   Dimensionless distance   yplus :  0.17410E-01 0.29379E+01
   Friction thermal sca.    tstar :  0.17397E-11 0.10463E+03
   Rough dim-less th. sca.  tplus :  0.12333E-01 0.20812E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21313E+00      11   0.85825E-05   0.30866E+02 0.11401E+03 
c  Velocity[X]                                      0.14674E+02 
c  Velocity[Y]                                      0.23887E+01 
c  Velocity[Z]                                      0.13803E+02 
c  Pressure     0.33733E-04      21   0.69308E-03   0.38187E-01 0.34745E+02 
c  k            0.11326E-02      15   0.31107E-03   0.38002E-01 0.19576E+03 
c  omega        0.27924E+07       1   0.45151E-06   0.94158E+08 0.14934E+01 
c  TempK        0.77664E+04       8   0.27855E-05   0.51394E+03 0.15934E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7482e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.459          18.319      -0.0013901      -0.0087945
v  Velocity[Y]             -15.453          14.079        0.057674        0.074401
v  Velocity[Z]               -25.5          18.451         -1.6884        -0.48175
v  ǁVelocityǁ          0.0010364          25.675          6.9103          5.7207
v  Pressure                -517.48          197.75          22.346          32.281
v  k                    4.425e-012          6.0083        0.025304        0.037659
v  omega                    14.677     2.7337e+008     1.2903e+006           76132
v  TempK                    298.15          363.17          317.28          315.37
v  TurbVisc            1.1136e-019      0.00063027     8.5421e-006     2.9341e-005
v  CourantNb           5.5274e-005          1.1431         0.77379         0.97117
v  FourierNb             0.0028738               1         0.38633        0.097901
v  total_pressure      1.0081e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0065071     8.8339e-005      0.00023504

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.66           305.5
v  Yplus               0          2.9379         0.57282          0.4227


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46721               2          1.1601          1.0691


 INSTANT    0.169000000E-02   TIME STEP NUMBER             169
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924476E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25341E-01 0.46994E+01
   Friction velocity        uk    :  0.25341E-01 0.46954E+01
   Dimensionless distance   yplus :  0.17182E-01 0.29378E+01
   Friction thermal sca.    tstar :  0.22340E-11 0.10629E+03
   Rough dim-less th. sca.  tplus :  0.12172E-01 0.20812E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21360E+00      11   0.85601E-05   0.30595E+02 0.11303E+03 
c  Velocity[X]                                      0.14510E+02 
c  Velocity[Y]                                      0.23642E+01 
c  Velocity[Z]                                      0.13721E+02 
c  Pressure     0.33566E-04      21   0.68624E-03   0.37952E-01 0.34511E+02 
c  k            0.11580E-02      15   0.30175E-03   0.38282E-01 0.19305E+03 
c  omega        0.27924E+07       1   0.44965E-06   0.86778E+08 0.14315E+01 
c  TempK        0.77812E+04       8   0.27825E-05   0.50823E+03 0.15739E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7552e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.453            18.3      -0.0013621      -0.0088348
v  Velocity[Y]             -15.379          14.021        0.057705        0.074504
v  Velocity[Z]             -25.498           18.46         -1.6882        -0.48163
v  ǁVelocityǁ         0.00074888          25.674           6.919          5.7314
v  Pressure                -516.26          197.87          22.405          32.265
v  k                   4.4379e-012          6.0617          0.0257        0.038364
v  omega                    14.885     2.7337e+008     1.2903e+006           76139
v  TempK                    298.15          363.17          317.37          315.44
v  TurbVisc            1.1166e-019      0.00061545     8.6319e-006      2.957e-005
v  CourantNb           5.5912e-005          1.1422           0.774         0.97129
v  FourierNb             0.0028723               1         0.38625        0.097823
v  total_pressure      1.0081e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0061906     8.8111e-005      0.00023443

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.67           305.5
v  Yplus               0          2.9378         0.57322         0.42314


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51833               2          1.1602          1.0691


 INSTANT    0.170000000E-02   TIME STEP NUMBER             170
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924507E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24963E-01 0.46996E+01
   Friction velocity        uk    :  0.24963E-01 0.46956E+01
   Dimensionless distance   yplus :  0.16925E-01 0.29377E+01
   Friction thermal sca.    tstar :  0.28851E-11 0.10787E+03
   Rough dim-less th. sca.  tplus :  0.11990E-01 0.20811E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21406E+00      11   0.85514E-05   0.30324E+02 0.11207E+03 
c  Velocity[X]                                      0.14344E+02 
c  Velocity[Y]                                      0.23478E+01 
c  Velocity[Z]                                      0.13632E+02 
c  Pressure     0.33376E-04      21   0.68697E-03   0.37695E-01 0.34477E+02 
c  k            0.11836E-02      15   0.29298E-03   0.38569E-01 0.19057E+03 
c  omega        0.27924E+07       1   0.44782E-06   0.81774E+08 0.13874E+01 
c  TempK        0.77960E+04       8   0.27796E-05   0.50260E+03 0.15543E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7619e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.446          18.282      -0.0013251      -0.0088678
v  Velocity[Y]             -15.362          13.987        0.057726        0.074601
v  Velocity[Z]             -25.496          18.402         -1.6879        -0.48152
v  ǁVelocityǁ         0.00047173          25.673          6.9277          5.7421
v  Pressure                   -515          198.01          22.475          32.261
v  k                   4.4519e-012          6.1178        0.026098        0.039069
v  omega                    15.097     2.7337e+008     1.2903e+006           76147
v  TempK                    298.15          363.17          317.46           315.5
v  TurbVisc            1.1198e-019       0.0005978     8.7193e-006     2.9791e-005
v  CourantNb           5.5597e-005          1.1413         0.77422         0.97141
v  FourierNb              0.002872               1         0.38615        0.097726
v  total_pressure      1.0081e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0068097     8.7885e-005      0.00023383

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.67           305.5
v  Yplus               0          2.9377         0.57362         0.42359


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57859               2          1.1604          1.0691


 INSTANT    0.171000000E-02   TIME STEP NUMBER             171
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924361E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24618E-01 0.46998E+01
   Friction velocity        uk    :  0.24618E-01 0.46958E+01
   Dimensionless distance   yplus :  0.16692E-01 0.29376E+01
   Friction thermal sca.    tstar :  0.37399E-11 0.10935E+03
   Rough dim-less th. sca.  tplus :  0.11824E-01 0.20810E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21452E+00      11   0.85040E-05   0.30053E+02 0.11109E+03 
c  Velocity[X]                                      0.14172E+02 
c  Velocity[Y]                                      0.23319E+01 
c  Velocity[Z]                                      0.13550E+02 
c  Pressure     0.33369E-04      21   0.68267E-03   0.37643E-01 0.34616E+02 
c  k            0.12095E-02      15   0.28513E-03   0.39042E-01 0.18948E+03 
c  omega        0.27924E+07       1   0.44635E-06   0.83027E+08 0.13945E+01 
c  TempK        0.78107E+04       8   0.27773E-05   0.49703E+03 0.15347E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7677e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.438          18.264       -0.001287      -0.0089032
v  Velocity[Y]             -15.416          13.979        0.057737        0.074695
v  Velocity[Z]             -25.495          18.409         -1.6877        -0.48142
v  ǁVelocityǁ         0.00034724          25.672          6.9364          5.7527
v  Pressure                 -513.7          198.15          22.557           32.27
v  k                   4.4674e-012          6.1767        0.026498        0.039773
v  omega                    15.313     2.7338e+008     1.2903e+006           76154
v  TempK                    298.15          363.17          317.55          315.57
v  TurbVisc            1.1233e-019      0.00057821     8.8053e-006     3.0007e-005
v  CourantNb           5.4552e-005          1.1405         0.77442         0.97151
v  FourierNb             0.0028727               1         0.38605        0.097611
v  total_pressure      1.0081e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0074907     8.7662e-005      0.00023326

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.67          305.51
v  Yplus               0          2.9376         0.57403         0.42404


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61216               2          1.1605          1.0691


 INSTANT    0.172000000E-02   TIME STEP NUMBER             172
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924432E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21716E-01 0.47000E+01
   Friction velocity        uk    :  0.21716E-01 0.46960E+01
   Dimensionless distance   yplus :  0.15582E-01 0.29376E+01
   Friction thermal sca.    tstar :  0.51646E-11 0.11073E+03
   Rough dim-less th. sca.  tplus :  0.11038E-01 0.20810E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21498E+00      11   0.84370E-05   0.29790E+02 0.11015E+03 
c  Velocity[X]                                      0.14009E+02 
c  Velocity[Y]                                      0.23181E+01 
c  Velocity[Z]                                      0.13463E+02 
c  Pressure     0.33223E-04      20   0.67854E-03   0.37435E-01 0.33829E+02 
c  k            0.12356E-02      15   0.27740E-03   0.39782E-01 0.19019E+03 
c  omega        0.27924E+07       1   0.44488E-06   0.85280E+08 0.14099E+01 
c  TempK        0.78255E+04       8   0.27751E-05   0.49153E+03 0.15152E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7724e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.43          18.248      -0.0012444      -0.0089464
v  Velocity[Y]             -15.483          13.986        0.057738        0.074781
v  Velocity[Z]             -25.493          18.354         -1.6873        -0.48132
v  ǁVelocityǁ          0.0004175          25.672          6.9451          5.7633
v  Pressure                -512.34          198.28          22.628          32.266
v  k                    4.484e-012          6.2385        0.026902        0.040477
v  omega                    15.533     2.7338e+008     1.2903e+006           76160
v  TempK                    298.15          363.17          317.64          315.64
v  TurbVisc            1.1272e-019      0.00056769     8.8916e-006     3.0222e-005
v  CourantNb            5.734e-005          1.1399         0.77463         0.97161
v  FourierNb             0.0028743               1         0.38594        0.097489
v  total_pressure      1.0081e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0070863      8.744e-005      0.00023269

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.68          305.51
v  Yplus               0          2.9376         0.57445         0.42449


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60793               2          1.1606          1.0691


 INSTANT    0.173000000E-02   TIME STEP NUMBER             173
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924377E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23933E-01 0.47002E+01
   Friction velocity        uk    :  0.23933E-01 0.46961E+01
   Dimensionless distance   yplus :  0.16295E-01 0.29375E+01
   Friction thermal sca.    tstar :  0.65829E-11 0.11196E+03
   Rough dim-less th. sca.  tplus :  0.11543E-01 0.20809E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21544E+00      11   0.83611E-05   0.29528E+02 0.10924E+03 
c  Velocity[X]                                      0.13849E+02 
c  Velocity[Y]                                      0.23047E+01 
c  Velocity[Z]                                      0.13375E+02 
c  Pressure     0.32890E-04      21   0.67959E-03   0.37019E-01 0.33335E+02 
c  k            0.12620E-02      15   0.27047E-03   0.40702E-01 0.19193E+03 
c  omega        0.27924E+07       1   0.44329E-06   0.88050E+08 0.14325E+01 
c  TempK        0.78403E+04       8   0.27730E-05   0.48612E+03 0.14958E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7779e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.422          18.232      -0.0012071      -0.0089903
v  Velocity[Y]             -15.439          14.379        0.057737        0.074853
v  Velocity[Z]             -25.492          18.364          -1.687        -0.48122
v  ǁVelocityǁ         0.00048765          25.671          6.9537          5.7739
v  Pressure                -510.95          198.39          22.693          32.256
v  k                   4.5025e-012          6.3029         0.02731         0.04118
v  omega                    15.753     2.7338e+008     1.2903e+006           76167
v  TempK                    298.15          363.17          317.73           315.7
v  TurbVisc            1.1314e-019      0.00056699     8.9785e-006     3.0435e-005
v  CourantNb           6.0186e-005          1.1392         0.77482          0.9717
v  FourierNb             0.0028767               1         0.38584        0.097361
v  total_pressure      1.0081e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0065355     8.7223e-005      0.00023214

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.68          305.51
v  Yplus               0          2.9375         0.57487         0.42493


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49119               2          1.1607          1.0691


 INSTANT    0.174000000E-02   TIME STEP NUMBER             174
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924476E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23772E-01 0.47004E+01
   Friction velocity        uk    :  0.23772E-01 0.46963E+01
   Dimensionless distance   yplus :  0.16118E-01 0.29374E+01
   Friction thermal sca.    tstar :  0.85660E-11 0.11316E+03
   Rough dim-less th. sca.  tplus :  0.11418E-01 0.20809E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21589E+00      11   0.83027E-05   0.29280E+02 0.10835E+03 
c  Velocity[X]                                      0.13696E+02 
c  Velocity[Y]                                      0.22908E+01 
c  Velocity[Z]                                      0.13293E+02 
c  Pressure     0.32935E-04      21   0.67130E-03   0.37026E-01 0.32521E+02 
c  k            0.12886E-02      15   0.26298E-03   0.41729E-01 0.19400E+03 
c  omega        0.27924E+07       1   0.44193E-06   0.95008E+08 0.14877E+01 
c  TempK        0.78550E+04       8   0.27710E-05   0.48080E+03 0.14763E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7828e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.413          18.217      -0.0011677      -0.0090283
v  Velocity[Y]              -15.34          14.085        0.057732        0.074916
v  Velocity[Z]             -25.491          18.305         -1.6866        -0.48112
v  ǁVelocityǁ         0.00053208           25.67          6.9624          5.7845
v  Pressure                -509.51          198.49          22.741          32.229
v  k                   4.5232e-012          6.3696        0.027724        0.041884
v  omega                    15.978     2.7338e+008     1.2903e+006           76174
v  TempK                    298.15          363.17          317.81          315.77
v  TurbVisc            1.1361e-019      0.00057236     9.0669e-006     3.0649e-005
v  CourantNb           6.2756e-005          1.1386         0.77501         0.97178
v  FourierNb             0.0028799               1         0.38573        0.097233
v  total_pressure      1.0082e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0066183     8.7008e-005      0.00023161

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.68          305.51
v  Yplus               0          2.9374         0.57529         0.42537


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40262               2          1.1607           1.069


 INSTANT    0.175000000E-02   TIME STEP NUMBER             175
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924395E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23529E-01 0.47006E+01
   Friction velocity        uk    :  0.23529E-01 0.46966E+01
   Dimensionless distance   yplus :  0.15953E-01 0.29373E+01
   Friction thermal sca.    tstar :  0.11395E-10 0.11430E+03
   Rough dim-less th. sca.  tplus :  0.11301E-01 0.20808E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21635E+00      11   0.82349E-05   0.29022E+02 0.10746E+03 
c  Velocity[X]                                      0.13543E+02 
c  Velocity[Y]                                      0.22712E+01 
c  Velocity[Z]                                      0.13208E+02 
c  Pressure     0.32580E-04      21   0.66817E-03   0.36588E-01 0.31993E+02 
c  k            0.13155E-02      15   0.25928E-03   0.42768E-01 0.19583E+03 
c  omega        0.27924E+07       1   0.43916E-06   0.79544E+08 0.13664E+01 
c  TempK        0.78698E+04       8   0.27691E-05   0.47555E+03 0.14570E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7876e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.403          18.202      -0.0011294      -0.0090655
v  Velocity[Y]             -15.316          14.013        0.057725        0.074975
v  Velocity[Z]             -25.491          18.315         -1.6861        -0.48102
v  ǁVelocityǁ         0.00075433          25.669           6.971           5.795
v  Pressure                -508.07          198.58           22.78          32.195
v  k                   4.5463e-012          6.4383        0.028143        0.042587
v  omega                    16.208     2.7338e+008     1.2903e+006           76181
v  TempK                    298.15          363.17           317.9          315.84
v  TurbVisc            1.1413e-019      0.00057433     9.1559e-006     3.0863e-005
v  CourantNb           6.4138e-005           1.138         0.77519         0.97186
v  FourierNb             0.0028838               1         0.38563        0.097102
v  total_pressure      1.0082e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0066762     8.6793e-005      0.00023108

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.69          305.51
v  Yplus               0          2.9373          0.5757         0.42581


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62748               2          1.1608           1.069


 INSTANT    0.176000000E-02   TIME STEP NUMBER             176
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924337E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23329E-01 0.47008E+01
   Friction velocity        uk    :  0.23329E-01 0.46968E+01
   Dimensionless distance   yplus :  0.15818E-01 0.29372E+01
   Friction thermal sca.    tstar :  0.14497E-10 0.11525E+03
   Rough dim-less th. sca.  tplus :  0.11205E-01 0.20807E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21681E+00      11   0.81558E-05   0.28765E+02 0.10659E+03 
c  Velocity[X]                                      0.13391E+02 
c  Velocity[Y]                                      0.22565E+01 
c  Velocity[Z]                                      0.13117E+02 
c  Pressure     0.32288E-04      21   0.66492E-03   0.36220E-01 0.31739E+02 
c  k            0.13426E-02      15   0.25700E-03   0.43593E-01 0.19641E+03 
c  omega        0.27924E+07       1   0.43730E-06   0.77107E+08 0.13459E+01 
c  TempK        0.78845E+04       8   0.27674E-05   0.47035E+03 0.14377E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      8.792e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.394          18.189       -0.001093      -0.0091015
v  Velocity[Y]             -15.346          13.987        0.057715        0.075029
v  Velocity[Z]              -25.49          18.257         -1.6857        -0.48092
v  ǁVelocityǁ           0.000804          25.668          6.9797          5.8055
v  Pressure                -506.58          198.66          22.818          32.158
v  k                   4.5721e-012          6.5086         0.02857        0.043291
v  omega                    16.444     2.7338e+008     1.2903e+006           76187
v  TempK                    298.15          363.17          317.99          315.92
v  TurbVisc            1.1471e-019       0.0005734     9.2455e-006     3.1076e-005
v  CourantNb            5.475e-005          1.1374         0.77538         0.97194
v  FourierNb             0.0028885               1         0.38553        0.096971
v  total_pressure      1.0082e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0066824      8.658e-005      0.00023057

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.69          305.51
v  Yplus               0          2.9372         0.57612         0.42624


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6024               2          1.1609          1.0689


 INSTANT    0.177000000E-02   TIME STEP NUMBER             177
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924277E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22826E-01 0.47010E+01
   Friction velocity        uk    :  0.22826E-01 0.46969E+01
   Dimensionless distance   yplus :  0.15477E-01 0.29371E+01
   Friction thermal sca.    tstar :  0.18439E-10 0.11608E+03
   Rough dim-less th. sca.  tplus :  0.10964E-01 0.20807E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21726E+00      11   0.81367E-05   0.28509E+02 0.10573E+03 
c  Velocity[X]                                      0.13238E+02 
c  Velocity[Y]                                      0.22441E+01 
c  Velocity[Z]                                      0.13028E+02 
c  Pressure     0.32075E-04      21   0.66096E-03   0.35945E-01 0.31452E+02 
c  k            0.13700E-02      15   0.25423E-03   0.44231E-01 0.19634E+03 
c  omega        0.27924E+07       1   0.43627E-06   0.82362E+08 0.13822E+01 
c  TempK        0.78993E+04       8   0.27655E-05   0.46518E+03 0.14185E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7953e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.384          18.177      -0.0010593      -0.0091308
v  Velocity[Y]             -15.469          13.997          0.0577        0.075086
v  Velocity[Z]              -25.49          18.265         -1.6851        -0.48084
v  ǁVelocityǁ         0.00082665          25.668          6.9883          5.8159
v  Pressure                -505.08          198.73          22.851          32.117
v  k                    4.601e-012          6.5803        0.029003        0.043996
v  omega                    16.686     2.7339e+008     1.2903e+006           76194
v  TempK                    298.15          363.17          318.08          315.99
v  TurbVisc            1.1537e-019      0.00056991     9.3361e-006      3.129e-005
v  CourantNb           5.6849e-005           1.137         0.77555         0.97202
v  FourierNb             0.0028939               1         0.38543        0.096845
v  total_pressure      1.0082e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0065299      8.637e-005      0.00023008

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.69          305.51
v  Yplus               0          2.9371         0.57654         0.42667


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58154               2           1.161          1.0689


 INSTANT    0.178000000E-02   TIME STEP NUMBER             178
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924479E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22299E-01 0.47011E+01
   Friction velocity        uk    :  0.22299E-01 0.46971E+01
   Dimensionless distance   yplus :  0.15119E-01 0.29370E+01
   Friction thermal sca.    tstar :  0.23500E-10 0.11674E+03
   Rough dim-less th. sca.  tplus :  0.10711E-01 0.20806E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21772E+00      11   0.80751E-05   0.28247E+02 0.10486E+03 
c  Velocity[X]                                      0.13068E+02 
c  Velocity[Y]                                      0.22349E+01 
c  Velocity[Z]                                      0.12944E+02 
c  Pressure     0.31753E-04      21   0.65175E-03   0.35550E-01 0.31152E+02 
c  k            0.13974E-02      15   0.25032E-03   0.44667E-01 0.19552E+03 
c  omega        0.27924E+07       1   0.43473E-06   0.84532E+08 0.13986E+01 
c  TempK        0.79141E+04       8   0.27634E-05   0.46003E+03 0.13993E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7986e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.374          18.165      -0.0010265      -0.0091629
v  Velocity[Y]             -15.502          14.024        0.057683        0.075138
v  Velocity[Z]              -25.49          18.204         -1.6846        -0.48076
v  ǁVelocityǁ         0.00082948          25.667          6.9969          5.8262
v  Pressure                -503.54          198.81          22.885          32.078
v  k                   4.6333e-012          6.6528        0.029441        0.044701
v  omega                    16.933     2.7339e+008     1.2903e+006           76200
v  TempK                    298.15          363.17          318.16          316.06
v  TurbVisc            1.1609e-019      0.00057539     9.4276e-006     3.1504e-005
v  CourantNb           5.9701e-005          1.1365         0.77573         0.97209
v  FourierNb                0.0029               1         0.38534         0.09672
v  total_pressure      1.0082e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0063046     8.6164e-005      0.00022959

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           303.7          305.51
v  Yplus               0           2.937         0.57696          0.4271


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56004               2          1.1611          1.0688


 INSTANT    0.179000000E-02   TIME STEP NUMBER             179
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924540E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21783E-01 0.47013E+01
   Friction velocity        uk    :  0.21783E-01 0.46973E+01
   Dimensionless distance   yplus :  0.14769E-01 0.29370E+01
   Friction thermal sca.    tstar :  0.30240E-10 0.11731E+03
   Rough dim-less th. sca.  tplus :  0.10462E-01 0.20806E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21817E+00      11   0.80001E-05   0.27973E+02 0.10396E+03 
c  Velocity[X]                                      0.12889E+02 
c  Velocity[Y]                                      0.22242E+01 
c  Velocity[Z]                                      0.12861E+02 
c  Pressure     0.31601E-04      21   0.64421E-03   0.35349E-01 0.30912E+02 
c  k            0.14250E-02      15   0.25152E-03   0.44931E-01 0.19410E+03 
c  omega        0.27924E+07       1   0.43311E-06   0.80758E+08 0.13663E+01 
c  TempK        0.79289E+04       8   0.27612E-05   0.45497E+03 0.13802E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8027e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.365          18.155     -0.00099821       -0.009196
v  Velocity[Y]              -15.42          14.155        0.057667        0.075188
v  Velocity[Z]             -25.489          18.211          -1.684        -0.48068
v  ǁVelocityǁ         0.00083579          25.667          7.0055          5.8365
v  Pressure                   -502          198.89          22.921          32.041
v  k                   4.6694e-012          6.7256        0.029885        0.045408
v  omega                     17.18     2.7339e+008     1.2903e+006           76206
v  TempK                    298.15          363.17          318.25          316.14
v  TurbVisc            1.1691e-019      0.00058118     9.5217e-006     3.1719e-005
v  CourantNb           6.1992e-005           1.136         0.77591         0.97215
v  FourierNb             0.0028838               1         0.38525        0.096601
v  total_pressure      1.0082e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0062126      8.596e-005      0.00022912

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           303.7          305.52
v  Yplus               0           2.937         0.57738         0.42752


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53716               2          1.1612          1.0687


 INSTANT    0.180000000E-02   TIME STEP NUMBER             180
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924578E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21268E-01 0.47015E+01
   Friction velocity        uk    :  0.21268E-01 0.46975E+01
   Dimensionless distance   yplus :  0.14420E-01 0.29369E+01
   Friction thermal sca.    tstar :  0.38363E-10 0.11929E+03
   Rough dim-less th. sca.  tplus :  0.10215E-01 0.20805E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21862E+00      11   0.79341E-05   0.27691E+02 0.10304E+03 
c  Velocity[X]                                      0.12707E+02 
c  Velocity[Y]                                      0.22185E+01 
c  Velocity[Z]                                      0.12765E+02 
c  Pressure     0.31494E-04      21   0.64257E-03   0.35202E-01 0.30495E+02 
c  k            0.14526E-02      15   0.24787E-03   0.45153E-01 0.19257E+03 
c  omega        0.27924E+07       1   0.43186E-06   0.89998E+08 0.14375E+01 
c  TempK        0.79436E+04       8   0.27592E-05   0.44999E+03 0.13612E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      8.807e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.355          18.147     -0.00097032      -0.0092387
v  Velocity[Y]             -15.373          14.141        0.057649        0.075237
v  Velocity[Z]             -25.489          18.145         -1.6833        -0.48061
v  ǁVelocityǁ         0.00084596          25.666           7.014          5.8468
v  Pressure                -500.46          198.96          22.954          32.001
v  k                   4.7098e-012          6.7983        0.030337        0.046116
v  omega                     17.43     2.7339e+008     1.2903e+006           76212
v  TempK                    298.15          363.17          318.33          316.21
v  TurbVisc            1.1782e-019      0.00058382     9.6183e-006     3.1937e-005
v  CourantNb           5.8899e-005          1.1355         0.77608          0.9722
v  FourierNb             0.0028489               1         0.38516        0.096482
v  total_pressure      1.0082e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0059881     8.5754e-005      0.00022863

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           303.7          305.52
v  Yplus               0          2.9369         0.57781         0.42795


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51986               2          1.1612          1.0687


 INSTANT    0.181000000E-02   TIME STEP NUMBER             181
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924930E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20772E-01 0.47016E+01
   Friction velocity        uk    :  0.20772E-01 0.46976E+01
   Dimensionless distance   yplus :  0.14084E-01 0.29368E+01
   Friction thermal sca.    tstar :  0.48708E-10 0.12211E+03
   Rough dim-less th. sca.  tplus :  0.99772E-02 0.20805E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21907E+00      11   0.78702E-05   0.27397E+02 0.10210E+03 
c  Velocity[X]                                      0.12520E+02 
c  Velocity[Y]                                      0.22061E+01 
c  Velocity[Z]                                      0.12671E+02 
c  Pressure     0.31081E-04      21   0.63298E-03   0.34716E-01 0.29823E+02 
c  k            0.14803E-02      14   0.24186E-03   0.45680E-01 0.19280E+03 
c  omega        0.27924E+07       1   0.42880E-06   0.74835E+08 0.13125E+01 
c  TempK        0.79584E+04       8   0.27571E-05   0.44509E+03 0.13423E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8111e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.346          18.143      -0.0009391      -0.0092733
v  Velocity[Y]             -15.372          14.069        0.057629        0.075275
v  Velocity[Z]             -25.488          18.145         -1.6826        -0.48054
v  ǁVelocityǁ         0.00083233          25.666          7.0226           5.857
v  Pressure                   -499             199          22.966          31.942
v  k                   4.7549e-012          6.8702        0.030794        0.046824
v  omega                    17.687     2.7339e+008     1.2904e+006           76219
v  TempK                    298.15          363.17          318.42          316.29
v  TurbVisc            1.1884e-019      0.00057704     9.7172e-006     3.2155e-005
v  CourantNb           5.0633e-005          1.1349         0.77625         0.97225
v  FourierNb             0.0028162               1         0.38508        0.096365
v  total_pressure      1.0083e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0065869     8.5547e-005      0.00022815

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.71          305.52
v  Yplus               0          2.9368         0.57823         0.42837


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48928               2          1.1613          1.0686


 INSTANT    0.182000000E-02   TIME STEP NUMBER             182
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924997E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20298E-01 0.47018E+01
   Friction velocity        uk    :  0.20298E-01 0.46978E+01
   Dimensionless distance   yplus :  0.13762E-01 0.29368E+01
   Friction thermal sca.    tstar :  0.61831E-10 0.12495E+03
   Rough dim-less th. sca.  tplus :  0.97492E-02 0.20804E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21952E+00      11   0.77966E-05   0.27109E+02 0.10117E+03 
c  Velocity[X]                                      0.12329E+02 
c  Velocity[Y]                                      0.21960E+01 
c  Velocity[Z]                                      0.12584E+02 
c  Pressure     0.31222E-04      21   0.63349E-03   0.34849E-01 0.29572E+02 
c  k            0.15079E-02      14   0.23903E-03   0.46483E-01 0.19421E+03 
c  omega        0.27924E+07       1   0.42671E-06   0.75580E+08 0.13164E+01 
c  TempK        0.79731E+04       8   0.27546E-05   0.44025E+03 0.13236E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8147e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.338           18.14     -0.00090141       -0.009298
v  Velocity[Y]              -15.47          14.044        0.057604        0.075309
v  Velocity[Z]             -25.488          18.075         -1.6819        -0.48047
v  ǁVelocityǁ         0.00068636          25.666          7.0311          5.8672
v  Pressure                -497.58          199.04          22.975          31.879
v  k                   4.8052e-012          6.9409         0.03126        0.047533
v  omega                    17.948     2.7339e+008     1.2904e+006           76225
v  TempK                    298.15          363.17           318.5          316.37
v  TurbVisc            1.1998e-019      0.00056443     9.8185e-006     3.2375e-005
v  CourantNb           2.8218e-005          1.1345         0.77642         0.97229
v  FourierNb             0.0027854               1           0.385        0.096256
v  total_pressure      1.0083e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0070557     8.5342e-005      0.00022767

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.71          305.52
v  Yplus               0          2.9368         0.57867         0.42879


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.2995               2          1.1614          1.0686


 INSTANT    0.183000000E-02   TIME STEP NUMBER             183
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925212E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19848E-01 0.47019E+01
   Friction velocity        uk    :  0.19848E-01 0.46979E+01
   Dimensionless distance   yplus :  0.13457E-01 0.29368E+01
   Friction thermal sca.    tstar :  0.78285E-10 0.12776E+03
   Rough dim-less th. sca.  tplus :  0.95331E-02 0.20804E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.21997E+00      11   0.77399E-05   0.26832E+02 0.10029E+03 
c  Velocity[X]                                      0.12143E+02 
c  Velocity[Y]                                      0.21910E+01 
c  Velocity[Z]                                      0.12498E+02 
c  Pressure     0.30927E-04      21   0.62349E-03   0.34499E-01 0.29338E+02 
c  k            0.15355E-02      14   0.23494E-03   0.47385E-01 0.19599E+03 
c  omega        0.27924E+07       1   0.42476E-06   0.82249E+08 0.13708E+01 
c  TempK        0.79878E+04       8   0.27516E-05   0.43547E+03 0.13049E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8182e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.33          18.139     -0.00085244      -0.0093161
v  Velocity[Y]              -15.52          14.054        0.057576         0.07534
v  Velocity[Z]             -25.486          18.069         -1.6811         -0.4804
v  ǁVelocityǁ         0.00053607          25.666          7.0396          5.8773
v  Pressure                -496.14          199.06          22.969          31.802
v  k                   4.8615e-012          7.0099        0.031734        0.048244
v  omega                    18.215     2.7339e+008     1.2904e+006           76231
v  TempK                    298.15          363.17          318.59          316.45
v  TurbVisc            1.2125e-019      0.00055547     9.9228e-006     3.2598e-005
v  CourantNb           1.2226e-005           1.134         0.77658         0.97235
v  FourierNb             0.0027565               1         0.38494        0.096153
v  total_pressure      1.0083e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0077613     8.5133e-005      0.00022717

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.71          305.52
v  Yplus               0          2.9368          0.5791         0.42921


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53444               2          1.1615          1.0685


 INSTANT    0.184000000E-02   TIME STEP NUMBER             184
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924900E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19420E-01 0.47021E+01
   Friction velocity        uk    :  0.19420E-01 0.46981E+01
   Dimensionless distance   yplus :  0.13167E-01 0.29367E+01
   Friction thermal sca.    tstar :  0.98339E-10 0.13056E+03
   Rough dim-less th. sca.  tplus :  0.93276E-02 0.20804E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22041E+00      11   0.76705E-05   0.26524E+02 0.99385E+02 
c  Velocity[X]                                      0.11957E+02 
c  Velocity[Y]                                      0.21862E+01 
c  Velocity[Z]                                      0.12381E+02 
c  Pressure     0.30646E-04      22   0.61536E-03   0.34166E-01 0.28956E+02 
c  k            0.15630E-02      14   0.23134E-03   0.48244E-01 0.19732E+03 
c  omega        0.27924E+07       1   0.42176E-06   0.73570E+08 0.12993E+01 
c  TempK        0.80025E+04       8   0.27486E-05   0.43076E+03 0.12864E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8225e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.323          18.138     -0.00079703      -0.0093281
v  Velocity[Y]             -15.441          14.079         0.05755        0.075366
v  Velocity[Z]             -25.485          17.994         -1.6803        -0.48034
v  ǁVelocityǁ         0.00038469          25.666          7.0481          5.8873
v  Pressure                -494.68           199.1          22.976          31.739
v  k                   4.9243e-012          7.0766        0.032218        0.048955
v  omega                    18.488     2.7339e+008     1.2904e+006           76236
v  TempK                    298.15          363.17          318.67          316.53
v  TurbVisc            1.2267e-019      0.00055254      1.003e-005     3.2823e-005
v  CourantNb           2.1015e-005          1.1335         0.77674          0.9724
v  FourierNb             0.0027293               1         0.38488        0.096054
v  total_pressure      1.0083e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0085374     8.4918e-005      0.00022665

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.72          305.52
v  Yplus               0          2.9367         0.57953         0.42964


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.31869               2          1.1616          1.0685


 INSTANT    0.185000000E-02   TIME STEP NUMBER             185
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924826E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18983E-01 0.47022E+01
   Friction velocity        uk    :  0.18983E-01 0.46982E+01
   Dimensionless distance   yplus :  0.12871E-01 0.29367E+01
   Friction thermal sca.    tstar :  0.12365E-09 0.13355E+03
   Rough dim-less th. sca.  tplus :  0.91179E-02 0.20804E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22086E+00      11   0.76025E-05   0.26229E+02 0.98494E+02 
c  Velocity[X]                                      0.11775E+02 
c  Velocity[Y]                                      0.21783E+01 
c  Velocity[Z]                                      0.12275E+02 
c  Pressure     0.30410E-04      24   0.61336E-03   0.33881E-01 0.28784E+02 
c  k            0.15906E-02      14   0.22882E-03   0.49192E-01 0.19901E+03 
c  omega        0.27924E+07       1   0.41898E-06   0.70167E+08 0.12664E+01 
c  TempK        0.80171E+04       8   0.27453E-05   0.42612E+03 0.12681E+02 
----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8265e-007                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.317          18.138     -0.00073432      -0.0093436
v  Velocity[Y]             -15.395          14.169        0.057526         0.07539
v  Velocity[Z]             -25.482          17.983         -1.6794        -0.48029
v  ǁVelocityǁ         0.00019755          25.667          7.0565          5.8973
v  Pressure                 -493.2          199.15          22.999          31.692
v  k                   4.9943e-012          7.1406        0.032711        0.049667
v  omega                    18.766     2.7339e+008     1.2904e+006           76242
v  TempK                    298.15          363.17          318.75          316.61
v  TurbVisc            1.2425e-019      0.00056193     1.0139e-005      3.305e-005
v  CourantNb           3.6515e-005          1.1329         0.77689         0.97245
v  FourierNb             0.0027037               1         0.38483        0.095959
v  total_pressure      1.0083e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0091127       8.47e-005      0.00022611

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.72          305.52
v  Yplus               0          2.9367         0.57997         0.43006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.36433               2          1.1617          1.0684


 INSTANT    0.186000000E-02   TIME STEP NUMBER             186
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925199E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16827E-01 0.47024E+01
   Friction velocity        uk    :  0.16827E-01 0.46984E+01
   Dimensionless distance   yplus :  0.12074E-01 0.29367E+01
   Friction thermal sca.    tstar :  0.15504E-09 0.13652E+03
   Rough dim-less th. sca.  tplus :  0.85535E-02 0.20804E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22130E+00      11   0.75296E-05   0.25940E+02 0.97639E+02 
c  Velocity[X]                                      0.11600E+02 
c  Velocity[Y]                                      0.21772E+01 
c  Velocity[Z]                                      0.12163E+02 
c  Pressure     0.30493E-04      24   0.60396E-03   0.33956E-01 0.28655E+02 
c  k            0.16181E-02      14   0.22557E-03   0.50010E-01 0.20002E+03 
c  omega        0.27924E+07       1   0.41726E-06   0.79419E+08 0.13438E+01 
c  TempK        0.80317E+04       8   0.27420E-05   0.42155E+03 0.12498E+02 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8305e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.315          18.139     -0.00065985      -0.0093529
v  Velocity[Y]             -15.401          14.191        0.057506        0.075414
v  Velocity[Z]              -25.48          17.909         -1.6786        -0.48025
v  ǁVelocityǁ         0.00010234          25.667          7.0649          5.9072
v  Pressure                -491.71          199.16          22.994          31.616
v  k                   5.0724e-012          7.2017        0.033214        0.050379
v  omega                     19.05      2.734e+008     1.2904e+006           76248
v  TempK                    298.15          363.17          318.84          316.69
v  TurbVisc            1.2602e-019      0.00057079     1.0251e-005     3.3277e-005
v  CourantNb           4.9919e-005          1.1324         0.77703          0.9725
v  FourierNb             0.0026797               1         0.38478        0.095869
v  total_pressure      1.0083e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0090412      8.448e-005      0.00022556

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.72          305.53
v  Yplus               0          2.9367         0.58041         0.43047


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54144               2          1.1618          1.0684


 INSTANT    0.187000000E-02   TIME STEP NUMBER             187
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925009E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11922E-01 0.47025E+01
   Friction velocity        uk    :  0.11922E-01 0.46985E+01
   Dimensionless distance   yplus :  0.85548E-02 0.29367E+01
   Friction thermal sca.    tstar :  0.19334E-09 0.13937E+03
   Rough dim-less th. sca.  tplus :  0.60603E-02 0.20804E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22174E+00      11   0.74730E-05   0.25651E+02 0.96775E+02 
c  Velocity[X]                                      0.11419E+02 
c  Velocity[Y]                                      0.21697E+01 
c  Velocity[Z]                                      0.12062E+02 
c  Pressure     0.29756E-04      24   0.60429E-03   0.33116E-01 0.28648E+02 
c  k            0.16455E-02      14   0.22329E-03   0.50631E-01 0.20028E+03 
c  omega        0.27924E+07       1   0.41471E-06   0.72450E+08 0.12831E+01 
c  TempK        0.80462E+04       8   0.27383E-05   0.41704E+03 0.12318E+02 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      8.834e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.313          18.141     -0.00057814      -0.0093506
v  Velocity[Y]             -15.504          14.118        0.057483        0.075431
v  Velocity[Z]              -25.48          17.902         -1.6776         -0.4802
v  ǁVelocityǁ         0.00034149          25.667          7.0732          5.9171
v  Pressure                -490.17          199.18          22.985          31.538
v  k                   5.1594e-012          7.2594        0.033726        0.051091
v  omega                    19.339      2.734e+008     1.2904e+006           76254
v  TempK                    298.15          363.17          318.92          316.77
v  TurbVisc            1.2799e-019      0.00057586     1.0366e-005     3.3507e-005
v  CourantNb           4.6928e-005           1.132         0.77718         0.97254
v  FourierNb             0.0026573               1         0.38474        0.095783
v  total_pressure      1.0083e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.008824     8.4258e-005      0.00022499

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.73          305.53
v  Yplus               0          2.9367         0.58084         0.43088


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4226               2          1.1619          1.0683


 INSTANT    0.188000000E-02   TIME STEP NUMBER             188
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925089E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17835E-01 0.47027E+01
   Friction velocity        uk    :  0.17835E-01 0.46986E+01
   Dimensionless distance   yplus :  0.12093E-01 0.29367E+01
   Friction thermal sca.    tstar :  0.24051E-09 0.14209E+03
   Rough dim-less th. sca.  tplus :  0.85665E-02 0.20804E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22218E+00      11   0.74129E-05   0.25358E+02 0.95916E+02 
c  Velocity[X]                                      0.11229E+02 
c  Velocity[Y]                                      0.21650E+01 
c  Velocity[Z]                                      0.11964E+02 
c  Pressure     0.29416E-04      22   0.59758E-03   0.32721E-01 0.28466E+02 
c  k            0.16728E-02      14   0.21893E-03   0.51070E-01 0.20000E+03 
c  omega        0.27924E+07       1   0.41303E-06   0.80808E+08 0.13528E+01 
c  TempK        0.80607E+04       8   0.27345E-05   0.41258E+03 0.12138E+02 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8373e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.312          18.144     -0.00048672      -0.0093441
v  Velocity[Y]             -15.552          14.093        0.057459        0.075445
v  Velocity[Z]             -25.481          17.827         -1.6767        -0.48016
v  ǁVelocityǁ         0.00059504          25.668          7.0815          5.9269
v  Pressure                 -488.6          199.19          22.976           31.46
v  k                   5.2576e-012          7.3134        0.034245        0.051801
v  omega                    19.633      2.734e+008     1.2904e+006           76259
v  TempK                    298.15          363.17             319          316.86
v  TurbVisc            1.3018e-019      0.00057869     1.0481e-005     3.3733e-005
v  CourantNb           4.3884e-005          1.1316         0.77732         0.97258
v  FourierNb             0.0026365               1         0.38471        0.095695
v  total_pressure      1.0084e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0085641     8.4035e-005      0.00022442

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.73          305.53
v  Yplus               0          2.9367         0.58128          0.4313


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41149               2           1.162          1.0683


 INSTANT    0.189000000E-02   TIME STEP NUMBER             189
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924989E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17507E-01 0.47028E+01
   Friction velocity        uk    :  0.17507E-01 0.46988E+01
   Dimensionless distance   yplus :  0.11870E-01 0.29368E+01
   Friction thermal sca.    tstar :  0.29571E-09 0.14474E+03
   Rough dim-less th. sca.  tplus :  0.84086E-02 0.20804E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22262E+00      11   0.73468E-05   0.25054E+02 0.95044E+02 
c  Velocity[X]                                      0.11036E+02 
c  Velocity[Y]                                      0.21604E+01 
c  Velocity[Z]                                      0.11858E+02 
c  Pressure     0.29341E-04      21   0.59156E-03   0.32622E-01 0.28238E+02 
c  k            0.17000E-02      14   0.21572E-03   0.51397E-01 0.19948E+03 
c  omega        0.27924E+07       1   0.40989E-06   0.69000E+08 0.12508E+01 
c  TempK        0.80752E+04       8   0.27303E-05   0.40822E+03 0.11960E+02 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8415e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.312          18.147     -0.00039478      -0.0093347
v  Velocity[Y]             -15.469          14.102        0.057436         0.07545
v  Velocity[Z]             -25.482          17.815         -1.6757        -0.48011
v  ǁVelocityǁ         0.00070319          25.669          7.0898          5.9366
v  Pressure                -487.11           199.2          22.962          31.378
v  k                    5.372e-012          7.3636        0.034771        0.052511
v  omega                    19.932      2.734e+008     1.2904e+006           76265
v  TempK                    298.15          363.17          319.08          316.94
v  TurbVisc            1.3266e-019      0.00057755     1.0598e-005     3.3959e-005
v  CourantNb           4.1208e-005           1.131         0.77747         0.97262
v  FourierNb             0.0026172               1         0.38469        0.095612
v  total_pressure      1.0084e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0092365     8.3813e-005      0.00022385

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.73          305.53
v  Yplus               0          2.9368         0.58171          0.4317


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55677               2          1.1622          1.0682


 INSTANT    0.190000000E-02   TIME STEP NUMBER             190
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925012E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17175E-01 0.47029E+01
   Friction velocity        uk    :  0.17175E-01 0.46989E+01
   Dimensionless distance   yplus :  0.11645E-01 0.29368E+01
   Friction thermal sca.    tstar :  0.36342E-09 0.14753E+03
   Rough dim-less th. sca.  tplus :  0.82492E-02 0.20805E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22305E+00      11   0.72785E-05   0.24741E+02 0.94143E+02 
c  Velocity[X]                                      0.10838E+02 
c  Velocity[Y]                                      0.21539E+01 
c  Velocity[Z]                                      0.11750E+02 
c  Pressure     0.29308E-04      21   0.58742E-03   0.32569E-01 0.27877E+02 
c  k            0.17270E-02      14   0.21172E-03   0.51730E-01 0.19923E+03 
c  omega        0.27924E+07       1   0.40726E-06   0.64436E+08 0.12078E+01 
c  TempK        0.80896E+04       8   0.27261E-05   0.40390E+03 0.11784E+02 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8456e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.312          18.151     -0.00029589      -0.0093272
v  Velocity[Y]             -15.424          14.126        0.057413        0.075443
v  Velocity[Z]             -25.483          17.741         -1.6746        -0.48008
v  ǁVelocityǁ         0.00092631          25.671          7.0981          5.9462
v  Pressure                -485.68           199.2          22.949          31.299
v  k                   5.5011e-012          7.4099        0.035303         0.05322
v  omega                    20.237      2.734e+008     1.2904e+006           76270
v  TempK                    298.15          363.17          319.17          317.03
v  TurbVisc            1.3555e-019      0.00058008     1.0717e-005     3.4184e-005
v  CourantNb           3.8462e-005          1.1305         0.77763         0.97266
v  FourierNb             0.0025992               1         0.38467         0.09553
v  total_pressure      1.0084e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0071915     8.3592e-005      0.00022328

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.73          305.53
v  Yplus               0          2.9368         0.58215         0.43211


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53432               2          1.1623          1.0682


 INSTANT    0.191000000E-02   TIME STEP NUMBER             191
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924948E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16866E-01 0.47031E+01
   Friction velocity        uk    :  0.16866E-01 0.46990E+01
   Dimensionless distance   yplus :  0.11435E-01 0.29369E+01
   Friction thermal sca.    tstar :  0.44506E-09 0.15021E+03
   Rough dim-less th. sca.  tplus :  0.81009E-02 0.20805E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22349E+00      11   0.72101E-05   0.24431E+02 0.93256E+02 
c  Velocity[X]                                      0.10639E+02 
c  Velocity[Y]                                      0.21510E+01 
c  Velocity[Z]                                      0.11641E+02 
c  Pressure     0.29049E-04      21   0.58114E-03   0.32262E-01 0.27446E+02 
c  k            0.17539E-02      14   0.20813E-03   0.52211E-01 0.19981E+03 
c  omega        0.27924E+07       1   0.40497E-06   0.65412E+08 0.12100E+01 
c  TempK        0.81039E+04       8   0.27217E-05   0.39964E+03 0.11609E+02 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8494e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.312          18.156     -0.00019172      -0.0093168
v  Velocity[Y]             -15.427          14.208        0.057394        0.075434
v  Velocity[Z]             -25.484          17.736         -1.6736        -0.48005
v  ǁVelocityǁ         0.00099301          25.672          7.1063          5.9558
v  Pressure                -484.23          199.22           22.95          31.234
v  k                   5.6447e-012          7.4522        0.035841        0.053927
v  omega                    20.547      2.734e+008     1.2904e+006           76275
v  TempK                    298.15          363.17          319.25          317.11
v  TurbVisc            1.3881e-019      0.00058893     1.0837e-005     3.4408e-005
v  CourantNb           3.5853e-005            1.13         0.77778         0.97271
v  FourierNb             0.0025826               1         0.38466        0.095452
v  total_pressure      1.0084e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0064599     8.3377e-005      0.00022272

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.74          305.53
v  Yplus               0          2.9369         0.58259         0.43251


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.34602               2          1.1624          1.0682


 INSTANT    0.192000000E-02   TIME STEP NUMBER             192
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925081E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16586E-01 0.47032E+01
   Friction velocity        uk    :  0.16586E-01 0.46992E+01
   Dimensionless distance   yplus :  0.11245E-01 0.29369E+01
   Friction thermal sca.    tstar :  0.54450E-09 0.15273E+03
   Rough dim-less th. sca.  tplus :  0.79663E-02 0.20805E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22392E+00      11   0.71427E-05   0.24120E+02 0.92378E+02 
c  Velocity[X]                                      0.10438E+02 
c  Velocity[Y]                                      0.21515E+01 
c  Velocity[Z]                                      0.11530E+02 
c  Pressure     0.28917E-04      20   0.58486E-03   0.32099E-01 0.27319E+02 
c  k            0.17806E-02      14   0.20411E-03   0.52792E-01 0.20070E+03 
c  omega        0.27924E+07       1   0.40347E-06   0.76963E+08 0.13146E+01 
c  TempK        0.81182E+04       8   0.27169E-05   0.39545E+03 0.11436E+02 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8527e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.313          18.161    -7.5517e-005      -0.0093029
v  Velocity[Y]             -15.519          14.227        0.057373        0.075422
v  Velocity[Z]             -25.485           17.68         -1.6725        -0.48002
v  ǁVelocityǁ          0.0010606          25.673          7.1144          5.9653
v  Pressure                -482.83          199.24          22.949          31.167
v  k                   5.8053e-012          7.4904        0.036384        0.054632
v  omega                    20.863      2.734e+008     1.2904e+006           76280
v  TempK                    298.15          363.17          319.33           317.2
v  TurbVisc            1.4243e-019      0.00059689     1.0958e-005     3.4629e-005
v  CourantNb             3.33e-005          1.1296         0.77793         0.97275
v  FourierNb             0.0025673               1         0.38466        0.095372
v  total_pressure      1.0084e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.006279     8.3165e-005      0.00022216

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.74          305.54
v  Yplus               0          2.9369         0.58303         0.43292


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40794               2          1.1626          1.0681


 INSTANT    0.193000000E-02   TIME STEP NUMBER             193
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924950E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16343E-01 0.47033E+01
   Friction velocity        uk    :  0.16342E-01 0.46993E+01
   Dimensionless distance   yplus :  0.11080E-01 0.29370E+01
   Friction thermal sca.    tstar :  0.66524E-09 0.15499E+03
   Rough dim-less th. sca.  tplus :  0.78495E-02 0.20806E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22435E+00      11   0.70764E-05   0.23812E+02 0.91499E+02 
c  Velocity[X]                                      0.10242E+02 
c  Velocity[Y]                                      0.21498E+01 
c  Velocity[Z]                                      0.11420E+02 
c  Pressure     0.28390E-04      21   0.57367E-03   0.31499E-01 0.27091E+02 
c  k            0.18072E-02      14   0.20018E-03   0.53573E-01 0.20234E+03 
c  omega        0.27924E+07       1   0.40057E-06   0.74646E+08 0.12951E+01 
c  TempK        0.81324E+04       8   0.27112E-05   0.39133E+03 0.11264E+02 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8556e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.314          18.167     5.1243e-005      -0.0092798
v  Velocity[Y]              -15.56          14.157        0.057347        0.075401
v  Velocity[Z]             -25.487           17.69         -1.6714        -0.47999
v  ǁVelocityǁ          0.0010596          25.674          7.1225          5.9747
v  Pressure                -481.44          199.26          22.949          31.102
v  k                   5.9849e-012          7.5246        0.036934        0.055335
v  omega                    21.184      2.734e+008     1.2904e+006           76286
v  TempK                    298.15          363.17          319.41          317.29
v  TurbVisc            1.4648e-019      0.00059017      1.108e-005     3.4849e-005
v  CourantNb           3.1844e-005          1.1292         0.77808         0.97279
v  FourierNb             0.0025532               1         0.38466        0.095294
v  total_pressure      1.0084e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0069069     8.2957e-005      0.00022161

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.74          305.54
v  Yplus               0           2.937         0.58347         0.43333


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47914               2          1.1627          1.0681


 INSTANT    0.194000000E-02   TIME STEP NUMBER             194
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924986E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16130E-01 0.47035E+01
   Friction velocity        uk    :  0.16130E-01 0.46995E+01
   Dimensionless distance   yplus :  0.10937E-01 0.29370E+01
   Friction thermal sca.    tstar :  0.81114E-09 0.15702E+03
   Rough dim-less th. sca.  tplus :  0.77475E-02 0.20806E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22477E+00      11   0.70097E-05   0.23509E+02 0.90637E+02 
c  Velocity[X]                                      0.10045E+02 
c  Velocity[Y]                                      0.21487E+01 
c  Velocity[Z]                                      0.11316E+02 
c  Pressure     0.27983E-04      21   0.56014E-03   0.31032E-01 0.26753E+02 
c  k            0.18337E-02      14   0.19598E-03   0.54407E-01 0.20415E+03 
c  omega        0.27924E+07       1   0.39693E-06   0.63601E+08 0.12016E+01 
c  TempK        0.81466E+04       8   0.27054E-05   0.38728E+03 0.11095E+02 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8594e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.315          18.172      0.00018571      -0.0092505
v  Velocity[Y]             -15.476           14.13        0.057323        0.075379
v  Velocity[Z]             -25.488          17.648         -1.6702        -0.47996
v  ǁVelocityǁ          0.0004018          25.675          7.1306           5.984
v  Pressure                -480.08          199.29          22.954          31.043
v  k                   6.1833e-012          7.5551        0.037491        0.056036
v  omega                    21.508      2.734e+008     1.2904e+006           76291
v  TempK                    298.15          363.17          319.49          317.38
v  TurbVisc            1.5102e-019      0.00058235     1.1203e-005     3.5066e-005
v  CourantNb           3.1409e-005          1.1288         0.77822         0.97283
v  FourierNb               0.00254               1         0.38467        0.095216
v  total_pressure      1.0084e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0063619     8.2751e-005      0.00022108

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.75          305.54
v  Yplus               0           2.937         0.58391         0.43373


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44562               2          1.1629           1.068


 INSTANT    0.195000000E-02   TIME STEP NUMBER             195
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925005E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15904E-01 0.47037E+01
   Friction velocity        uk    :  0.15904E-01 0.46996E+01
   Dimensionless distance   yplus :  0.10783E-01 0.29371E+01
   Friction thermal sca.    tstar :  0.98753E-09 0.15924E+03
   Rough dim-less th. sca.  tplus :  0.76389E-02 0.20807E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22519E+00      11   0.69486E-05   0.23196E+02 0.89792E+02 
c  Velocity[X]                                      0.98544E+01 
c  Velocity[Y]                                      0.21456E+01 
c  Velocity[Z]                                      0.11197E+02 
c  Pressure     0.27725E-04      20   0.55633E-03   0.30729E-01 0.26444E+02 
c  k            0.18602E-02      14   0.19124E-03   0.55225E-01 0.20582E+03 
c  omega        0.27924E+07       1   0.39373E-06   0.58992E+08 0.11646E+01 
c  TempK        0.81606E+04       8   0.26998E-05   0.38330E+03 0.10927E+02 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8627e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.317          18.179       0.0003298      -0.0092143
v  Velocity[Y]             -15.424          14.134        0.057296        0.075358
v  Velocity[Z]              -25.49          17.666          -1.669        -0.47993
v  ǁVelocityǁ         0.00091391          25.677          7.1386          5.9932
v  Pressure                -478.73          199.31          22.963          30.988
v  k                   6.4008e-012          7.5818        0.038054        0.056733
v  omega                    21.836      2.734e+008     1.2904e+006           76296
v  TempK                    298.15          363.17          319.57          317.47
v  TurbVisc            1.5602e-019      0.00057394     1.1326e-005      3.528e-005
v  CourantNb           3.1015e-005          1.1283         0.77836         0.97288
v  FourierNb             0.0025279               1         0.38467        0.095136
v  total_pressure      1.0085e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0068638     8.2551e-005      0.00022056

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.75          305.54
v  Yplus               0          2.9371         0.58435         0.43413


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.27213               2           1.163           1.068


 INSTANT    0.196000000E-02   TIME STEP NUMBER             196
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924991E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15709E-01 0.47038E+01
   Friction velocity        uk    :  0.15709E-01 0.46998E+01
   Dimensionless distance   yplus :  0.10651E-01 0.29372E+01
   Friction thermal sca.    tstar :  0.12007E-08 0.16120E+03
   Rough dim-less th. sca.  tplus :  0.75452E-02 0.20807E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22561E+00      11   0.68924E-05   0.22910E+02 0.88995E+02 
c  Velocity[X]                                      0.96765E+01 
c  Velocity[Y]                                      0.21458E+01 
c  Velocity[Z]                                      0.11088E+02 
c  Pressure     0.27559E-04      20   0.55583E-03   0.30527E-01 0.26320E+02 
c  k            0.18867E-02      14   0.18740E-03   0.55960E-01 0.20710E+03 
c  omega        0.27924E+07       1   0.39085E-06   0.57897E+08 0.11583E+01 
c  TempK        0.81746E+04       8   0.26936E-05   0.37939E+03 0.10762E+02 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8657e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.319          18.185      0.00047835       -0.009178
v  Velocity[Y]             -15.419          14.149        0.057271         0.07534
v  Velocity[Z]             -25.491          17.631         -1.6678        -0.47991
v  ǁVelocityǁ         0.00063889          25.679          7.1465          6.0024
v  Pressure                -477.39          199.35           22.98          30.943
v  k                   6.5076e-012          7.6051        0.038625        0.057428
v  omega                    22.167      2.734e+008     1.2904e+006           76301
v  TempK                    298.15          363.17          319.65          317.56
v  TurbVisc            1.6151e-019       0.0005793     1.1449e-005     3.5489e-005
v  CourantNb           3.0668e-005          1.1279          0.7785         0.97292
v  FourierNb              0.002517               1         0.38469        0.095056
v  total_pressure      1.0085e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0071191     8.2355e-005      0.00022005

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.75          305.54
v  Yplus               0          2.9372         0.58479         0.43453


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.34036               2          1.1632           1.068


 INSTANT    0.197000000E-02   TIME STEP NUMBER             197
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924624E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15541E-01 0.47040E+01
   Friction velocity        uk    :  0.15541E-01 0.46999E+01
   Dimensionless distance   yplus :  0.10537E-01 0.29373E+01
   Friction thermal sca.    tstar :  0.14573E-08 0.16293E+03
   Rough dim-less th. sca.  tplus :  0.74646E-02 0.20808E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22603E+00      11   0.68294E-05   0.22622E+02 0.88220E+02 
c  Velocity[X]                                      0.95009E+01 
c  Velocity[Y]                                      0.21463E+01 
c  Velocity[Z]                                      0.10975E+02 
c  Pressure     0.27229E-04      19   0.55460E-03   0.30143E-01 0.26326E+02 
c  k            0.19131E-02      14   0.18378E-03   0.56534E-01 0.20785E+03 
c  omega        0.27924E+07       1   0.38846E-06   0.60653E+08 0.11854E+01 
c  TempK        0.81886E+04       8   0.26871E-05   0.37555E+03 0.10598E+02 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8682e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.322          18.191      0.00063488      -0.0091356
v  Velocity[Y]             -15.494          14.171        0.057242        0.075319
v  Velocity[Z]             -25.493          17.662         -1.6666        -0.47988
v  ǁVelocityǁ           0.000913          25.681          7.1544          6.0115
v  Pressure                -476.04           199.4          23.012          30.914
v  k                   6.5968e-012          7.6251        0.039202        0.058119
v  omega                    22.501     2.7341e+008     1.2905e+006           76306
v  TempK                    298.15          363.17          319.73          317.65
v  TurbVisc            1.6486e-019      0.00058254     1.1572e-005     3.5693e-005
v  CourantNb           3.0274e-005          1.1276         0.77864         0.97297
v  FourierNb             0.0025071               1          0.3847        0.094974
v  total_pressure      1.0085e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0074149     8.2165e-005      0.00021956

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.75          305.55
v  Yplus               0          2.9373         0.58522         0.43493


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4566               2          1.1633          1.0679


 INSTANT    0.198000000E-02   TIME STEP NUMBER             198
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924736E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15409E-01 0.47041E+01
   Friction velocity        uk    :  0.15409E-01 0.47001E+01
   Dimensionless distance   yplus :  0.10447E-01 0.29374E+01
   Friction thermal sca.    tstar :  0.17665E-08 0.16431E+03
   Rough dim-less th. sca.  tplus :  0.74011E-02 0.20809E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22645E+00      11   0.67724E-05   0.22337E+02 0.87467E+02 
c  Velocity[X]                                      0.93209E+01 
c  Velocity[Y]                                      0.21479E+01 
c  Velocity[Z]                                      0.10869E+02 
c  Pressure     0.27081E-04      19   0.55143E-03   0.29960E-01 0.26371E+02 
c  k            0.19394E-02      14   0.17959E-03   0.56897E-01 0.20806E+03 
c  omega        0.27924E+07       1   0.38664E-06   0.68005E+08 0.12535E+01 
c  TempK        0.82025E+04       8   0.26804E-05   0.37178E+03 0.10436E+02 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8699e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.324          18.198      0.00079878      -0.0090845
v  Velocity[Y]             -15.542          14.235        0.057216        0.075297
v  Velocity[Z]             -25.495          17.643         -1.6654        -0.47987
v  ǁVelocityǁ         0.00088359          25.682          7.1622          6.0205
v  Pressure                 -474.7          199.46          23.054          30.894
v  k                    6.695e-012          7.6421        0.039784        0.058808
v  omega                    22.838     2.7341e+008     1.2905e+006           76311
v  TempK                    298.15          363.17          319.81          317.74
v  TurbVisc            1.6712e-019      0.00057621     1.1695e-005     3.5895e-005
v  CourantNb           2.9884e-005          1.1274         0.77877         0.97303
v  FourierNb             0.0024983               1         0.38472         0.09489
v  total_pressure      1.0085e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0074563     8.1979e-005      0.00021908

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.76          305.55
v  Yplus               0          2.9374         0.58566         0.43533


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44714               2          1.1635          1.0679


 INSTANT    0.199000000E-02   TIME STEP NUMBER             199
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924816E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15305E-01 0.47043E+01
   Friction velocity        uk    :  0.15305E-01 0.47003E+01
   Dimensionless distance   yplus :  0.10377E-01 0.29375E+01
   Friction thermal sca.    tstar :  0.21382E-08 0.16542E+03
   Rough dim-less th. sca.  tplus :  0.73512E-02 0.20809E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22686E+00      11   0.67145E-05   0.22051E+02 0.86709E+02 
c  Velocity[X]                                      0.91422E+01 
c  Velocity[Y]                                      0.21514E+01 
c  Velocity[Z]                                      0.10757E+02 
c  Pressure     0.27049E-04      19   0.53741E-03   0.29905E-01 0.25774E+02 
c  k            0.19657E-02      14   0.17376E-03   0.57107E-01 0.20798E+03 
c  omega        0.27924E+07       1   0.38427E-06   0.72626E+08 0.12885E+01 
c  TempK        0.82163E+04       8   0.26732E-05   0.36807E+03 0.10276E+02 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8726e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.326          18.205      0.00096793      -0.0090343
v  Velocity[Y]             -15.463          14.256        0.057193        0.075279
v  Velocity[Z]             -25.497          17.693         -1.6641        -0.47986
v  ǁVelocityǁ         0.00078219          25.684            7.17          6.0294
v  Pressure                -473.39           199.5          23.083          30.862
v  k                   6.8029e-012          7.6562         0.04037        0.059492
v  omega                    23.179     2.7341e+008     1.2905e+006           76315
v  TempK                    298.15          363.17          319.89          317.83
v  TurbVisc            1.6961e-019      0.00057144     1.1818e-005     3.6092e-005
v  CourantNb           3.0108e-005          1.1271         0.77891         0.97309
v  FourierNb             0.0024905               1         0.38474        0.094799
v  total_pressure      1.0085e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0067816     8.1793e-005      0.00021858

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.76          305.55
v  Yplus               0          2.9375         0.58609         0.43572


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38244               2          1.1637          1.0679


 INSTANT    0.200000000E-02   TIME STEP NUMBER             200
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924787E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15187E-01 0.47045E+01
   Friction velocity        uk    :  0.15187E-01 0.47004E+01
   Dimensionless distance   yplus :  0.10297E-01 0.29375E+01
   Friction thermal sca.    tstar :  0.25844E-08 0.16669E+03
   Rough dim-less th. sca.  tplus :  0.72943E-02 0.20810E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22728E+00      11   0.66460E-05   0.21741E+02 0.85896E+02 
c  Velocity[X]                                      0.89636E+01 
c  Velocity[Y]                                      0.21450E+01 
c  Velocity[Z]                                      0.10632E+02 
c  Pressure     0.26298E-04      19   0.53243E-03   0.29054E-01 0.25296E+02 
c  k            0.19919E-02      14   0.16944E-03   0.57238E-01 0.20787E+03 
c  omega        0.27924E+07       1   0.38054E-06   0.58216E+08 0.11501E+01 
c  TempK        0.82300E+04       8   0.26658E-05   0.36440E+03 0.10118E+02 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8746e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.329          18.211       0.0011395      -0.0089794
v  Velocity[Y]             -15.405          14.191        0.057172        0.075263
v  Velocity[Z]             -25.498          17.685         -1.6629        -0.47985
v  ǁVelocityǁ         0.00088557          25.686          7.1777          6.0382
v  Pressure                -472.11          199.53          23.103          30.823
v  k                   6.9209e-012          7.6678         0.04096        0.060173
v  omega                    23.423     2.7341e+008     1.2905e+006           76320
v  TempK                    298.15          363.17          319.97          317.92
v  TurbVisc            1.7234e-019      0.00056762      1.194e-005     3.6285e-005
v  CourantNb            3.173e-005          1.1268         0.77905         0.97314
v  FourierNb             0.0024837               1         0.38476        0.094706
v  total_pressure      1.0085e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0065237     8.1609e-005      0.00021809

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.76          305.55
v  Yplus               0          2.9375         0.58652         0.43611


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49014               2          1.1638          1.0678


 INSTANT    0.201000000E-02   TIME STEP NUMBER             201
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924568E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15090E-01 0.47046E+01
   Friction velocity        uk    :  0.15090E-01 0.47006E+01
   Dimensionless distance   yplus :  0.10231E-01 0.29376E+01
   Friction thermal sca.    tstar :  0.31199E-08 0.16775E+03
   Rough dim-less th. sca.  tplus :  0.72480E-02 0.20810E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22769E+00      11   0.65721E-05   0.21433E+02 0.85090E+02 
c  Velocity[X]                                      0.87737E+01 
c  Velocity[Y]                                      0.21419E+01 
c  Velocity[Z]                                      0.10518E+02 
c  Pressure     0.26008E-04      18   0.52830E-03   0.28712E-01 0.25114E+02 
c  k            0.20180E-02      14   0.16490E-03   0.57378E-01 0.20797E+03 
c  omega        0.27924E+07       1   0.37762E-06   0.55639E+08 0.11172E+01 
c  TempK        0.82437E+04       8   0.26586E-05   0.36080E+03 0.99623E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8762e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.332          18.218       0.0013139      -0.0089275
v  Velocity[Y]             -15.395          14.178        0.057152         0.07525
v  Velocity[Z]               -25.5          17.742         -1.6616        -0.47985
v  ǁVelocityǁ          0.0010077          25.687          7.1854           6.047
v  Pressure                -470.86          199.56          23.128          30.789
v  k                   7.0497e-012          7.6772        0.041551        0.060849
v  omega                    23.664     2.7341e+008     1.2905e+006           76325
v  TempK                    298.15          363.17          320.05          318.02
v  TurbVisc            1.7533e-019      0.00056369     1.2061e-005     3.6474e-005
v  CourantNb           3.3282e-005          1.1266          0.7792          0.9732
v  FourierNb             0.0024777               1         0.38479        0.094609
v  total_pressure      1.0085e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.007176     8.1429e-005       0.0002176

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.77          305.55
v  Yplus               0          2.9376         0.58694          0.4365


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4489               2           1.164          1.0678


 INSTANT    0.202000000E-02   TIME STEP NUMBER             202
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924456E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15032E-01 0.47048E+01
   Friction velocity        uk    :  0.15032E-01 0.47007E+01
   Dimensionless distance   yplus :  0.10192E-01 0.29377E+01
   Friction thermal sca.    tstar :  0.37616E-08 0.16839E+03
   Rough dim-less th. sca.  tplus :  0.72199E-02 0.20811E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22809E+00      11   0.64997E-05   0.21136E+02 0.84300E+02 
c  Velocity[X]                                      0.85829E+01 
c  Velocity[Y]                                      0.21415E+01 
c  Velocity[Z]                                      0.10411E+02 
c  Pressure     0.25613E-04      19   0.52329E-03   0.28254E-01 0.24848E+02 
c  k            0.20440E-02      14   0.15996E-03   0.57526E-01 0.20830E+03 
c  omega        0.27924E+07       1   0.37504E-06   0.56969E+08 0.11225E+01 
c  TempK        0.82572E+04       8   0.26504E-05   0.35725E+03 0.98085E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8771e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.334          18.225       0.0014889      -0.0088793
v  Velocity[Y]              -15.45          14.197        0.057133         0.07524
v  Velocity[Z]             -25.502           17.74         -1.6603        -0.47986
v  ǁVelocityǁ          0.0010019          25.689          7.1931          6.0557
v  Pressure                -469.63           199.6          23.153          30.755
v  k                   7.1898e-012          7.6846        0.042145        0.061521
v  omega                    23.918     2.7341e+008     1.2905e+006           76329
v  TempK                    298.15          363.17          320.12          318.11
v  TurbVisc             1.786e-019      0.00056019     1.2182e-005     3.6657e-005
v  CourantNb           3.1637e-005          1.1265         0.77935         0.97327
v  FourierNb             0.0024725               1         0.38481        0.094507
v  total_pressure      1.0086e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0078327     8.1248e-005       0.0002171

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.77          305.56
v  Yplus               0          2.9377         0.58737         0.43688


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.32899               2          1.1642          1.0678


 INSTANT    0.203000000E-02   TIME STEP NUMBER             203
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924155E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15001E-01 0.47049E+01
   Friction velocity        uk    :  0.15001E-01 0.47009E+01
   Dimensionless distance   yplus :  0.10171E-01 0.29378E+01
   Friction thermal sca.    tstar :  0.45293E-08 0.16872E+03
   Rough dim-less th. sca.  tplus :  0.72051E-02 0.20812E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22850E+00      11   0.64458E-05   0.20836E+02 0.83523E+02 
c  Velocity[X]                                      0.83939E+01 
c  Velocity[Y]                                      0.21425E+01 
c  Velocity[Z]                                      0.10300E+02 
c  Pressure     0.25651E-04      18   0.52042E-03   0.28272E-01 0.24922E+02 
c  k            0.20698E-02      14   0.15608E-03   0.57727E-01 0.20889E+03 
c  omega        0.27924E+07       1   0.37257E-06   0.59269E+08 0.11382E+01 
c  TempK        0.82708E+04       8   0.26422E-05   0.35376E+03 0.96568E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8772e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.337          18.232       0.0016637      -0.0088337
v  Velocity[Y]             -15.527          14.225        0.057113        0.075241
v  Velocity[Z]             -25.504          17.808         -1.6589        -0.47986
v  ǁVelocityǁ         0.00089702          25.691          7.2006          6.0643
v  Pressure                -468.43          199.65          23.191          30.736
v  k                   7.3421e-012          7.6904         0.04274        0.062189
v  omega                    24.187     2.7341e+008     1.2905e+006           76334
v  TempK                    298.15          363.17           320.2          318.21
v  TurbVisc            1.8215e-019      0.00055835     1.2301e-005     3.6836e-005
v  CourantNb           3.3939e-005          1.1265         0.77951         0.97333
v  FourierNb             0.0024679               1         0.38483        0.094397
v  total_pressure      1.0086e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.007247     8.1071e-005      0.00021661

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.77          305.56
v  Yplus               0          2.9378          0.5878         0.43726


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5184               2          1.1643          1.0677


 INSTANT    0.204000000E-02   TIME STEP NUMBER             204
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924220E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15004E-01 0.47051E+01
   Friction velocity        uk    :  0.15004E-01 0.47010E+01
   Dimensionless distance   yplus :  0.10173E-01 0.29379E+01
   Friction thermal sca.    tstar :  0.54467E-08 0.16868E+03
   Rough dim-less th. sca.  tplus :  0.72064E-02 0.20812E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22890E+00      11   0.63766E-05   0.20537E+02 0.82746E+02 
c  Velocity[X]                                      0.82041E+01 
c  Velocity[Y]                                      0.21443E+01 
c  Velocity[Z]                                      0.10189E+02 
c  Pressure     0.25282E-04      18   0.51438E-03   0.27843E-01 0.24609E+02 
c  k            0.20956E-02      14   0.15192E-03   0.57996E-01 0.20975E+03 
c  omega        0.27924E+07       1   0.36943E-06   0.56936E+08 0.11139E+01 
c  TempK        0.82842E+04       7   0.51062E-05   0.34739E+03 0.94711E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8783e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.34          18.241       0.0018354      -0.0087905
v  Velocity[Y]             -15.478          14.255        0.057094        0.075245
v  Velocity[Z]             -25.506          17.812         -1.6576        -0.47987
v  ǁVelocityǁ         0.00099128          25.693          7.2081          6.0728
v  Pressure                -467.26           199.7          23.231          30.719
v  k                   7.5072e-012          7.6949        0.043337        0.062853
v  omega                     24.47     2.7341e+008     1.2905e+006           76339
v  TempK                    298.15          363.17          320.28           318.3
v  TurbVisc              1.86e-019      0.00055591     1.2418e-005      3.701e-005
v  CourantNb           3.7302e-005          1.1263         0.77966         0.97339
v  FourierNb             0.0024638               1         0.38486        0.094283
v  total_pressure      1.0086e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0063724     8.0896e-005      0.00021613

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.78          305.56
v  Yplus               0          2.9379         0.58822         0.43764


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.499               2          1.1645          1.0677


 INSTANT    0.205000000E-02   TIME STEP NUMBER             205
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924194E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14980E-01 0.47052E+01
   Friction velocity        uk    :  0.14980E-01 0.47011E+01
   Dimensionless distance   yplus :  0.10157E-01 0.29380E+01
   Friction thermal sca.    tstar :  0.65135E-08 0.16894E+03
   Rough dim-less th. sca.  tplus :  0.71951E-02 0.20813E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22930E+00      11   0.62959E-05   0.20233E+02 0.81966E+02 
c  Velocity[X]                                      0.80159E+01 
c  Velocity[Y]                                      0.21402E+01 
c  Velocity[Z]                                      0.10077E+02 
c  Pressure     0.24770E-04      19   0.51238E-03   0.27255E-01 0.24403E+02 
c  k            0.21214E-02      14   0.14791E-03   0.58376E-01 0.21080E+03 
c  omega        0.27924E+07       1   0.36674E-06   0.58710E+08 0.11310E+01 
c  TempK        0.82976E+04       7   0.50883E-05   0.34403E+03 0.93254E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8789e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.343           18.25       0.0020054      -0.0087558
v  Velocity[Y]             -15.378          14.323        0.057081        0.075254
v  Velocity[Z]             -25.507          17.891         -1.6563        -0.47988
v  ǁVelocityǁ         0.00098637          25.695          7.2156          6.0813
v  Pressure                -466.06          199.75          23.271          30.704
v  k                    7.686e-012          7.6984        0.043936        0.063512
v  omega                     24.77     2.7341e+008     1.2905e+006           76343
v  TempK                    298.15          363.17          320.36           318.4
v  TurbVisc            1.9019e-019       0.0005512     1.2535e-005     3.7179e-005
v  CourantNb            3.556e-005          1.1263         0.77981         0.97345
v  FourierNb             0.0024603               1         0.38488        0.094165
v  total_pressure      1.0086e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0053857     8.0727e-005      0.00021568

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.78          305.56
v  Yplus               0           2.938         0.58864         0.43802


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35606               2          1.1647          1.0676


 INSTANT    0.206000000E-02   TIME STEP NUMBER             206
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924207E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14953E-01 0.47053E+01
   Friction velocity        uk    :  0.14953E-01 0.47012E+01
   Dimensionless distance   yplus :  0.10138E-01 0.29381E+01
   Friction thermal sca.    tstar :  0.77865E-08 0.16924E+03
   Rough dim-less th. sca.  tplus :  0.71820E-02 0.20813E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.22970E+00      11   0.62334E-05   0.19935E+02 0.81211E+02 
c  Velocity[X]                                      0.78362E+01 
c  Velocity[Y]                                      0.21415E+01 
c  Velocity[Z]                                      0.99577E+01 
c  Pressure     0.24478E-04      18   0.50880E-03   0.26909E-01 0.24082E+02 
c  k            0.21471E-02      14   0.14426E-03   0.58802E-01 0.21187E+03 
c  omega        0.27924E+07       1   0.36373E-06   0.60389E+08 0.11493E+01 
c  TempK        0.83109E+04       7   0.50699E-05   0.34073E+03 0.91822E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8789e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.346          18.258        0.002174      -0.0087258
v  Velocity[Y]              -15.35           14.34        0.057072         0.07527
v  Velocity[Z]             -25.509          17.904         -1.6549         -0.4799
v  ǁVelocityǁ         0.00098159          25.696           7.223          6.0896
v  Pressure                -464.92          199.79          23.307          30.685
v  k                   7.8793e-012          7.7013        0.044537        0.064167
v  omega                    25.087     2.7341e+008     1.2905e+006           76347
v  TempK                    298.15          363.17          320.43          318.49
v  TurbVisc            1.9472e-019      0.00054621      1.265e-005     3.7344e-005
v  CourantNb           3.2323e-005          1.1263         0.77997         0.97351
v  FourierNb             0.0024574               1          0.3849        0.094042
v  total_pressure      1.0086e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044601     8.0563e-005      0.00021523

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.78          305.56
v  Yplus               0          2.9381         0.58907          0.4384


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.24542               2          1.1649          1.0675


 INSTANT    0.207000000E-02   TIME STEP NUMBER             207
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924207E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14967E-01 0.47053E+01
   Friction velocity        uk    :  0.14967E-01 0.47013E+01
   Dimensionless distance   yplus :  0.10148E-01 0.29381E+01
   Friction thermal sca.    tstar :  0.92977E-08 0.16907E+03
   Rough dim-less th. sca.  tplus :  0.71887E-02 0.20814E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23010E+00      11   0.61646E-05   0.19637E+02 0.80446E+02 
c  Velocity[X]                                      0.76592E+01 
c  Velocity[Y]                                      0.21396E+01 
c  Velocity[Z]                                      0.98383E+01 
c  Pressure     0.24179E-04      18   0.50723E-03   0.26555E-01 0.24111E+02 
c  k            0.21727E-02      14   0.14038E-03   0.59152E-01 0.21263E+03 
c  omega        0.27924E+07       1   0.35984E-06   0.51359E+08 0.10603E+01 
c  TempK        0.83241E+04       7   0.50503E-05   0.33750E+03 0.90415E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8782e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.349          18.267        0.002341      -0.0086983
v  Velocity[Y]             -15.373          14.275        0.057064        0.075286
v  Velocity[Z]              -25.51          17.994         -1.6536        -0.47992
v  ǁVelocityǁ         0.00097725          25.697          7.2303          6.0979
v  Pressure                 -463.8          199.84          23.353          30.677
v  k                   8.0459e-012          7.7038         0.04514        0.064817
v  omega                    25.422     2.7341e+008     1.2905e+006           76352
v  TempK                    298.15          363.17          320.51          318.59
v  TurbVisc            1.9961e-019      0.00054016     1.2765e-005     3.7505e-005
v  CourantNb           3.6603e-005          1.1263         0.78012         0.97357
v  FourierNb             0.0024552               1         0.38492        0.093916
v  total_pressure      1.0086e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0041531     8.0403e-005       0.0002148

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.78          305.57
v  Yplus               0          2.9381         0.58949         0.43878


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46998               2           1.165          1.0675


 INSTANT    0.208000000E-02   TIME STEP NUMBER             208
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924244E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14981E-01 0.47054E+01
   Friction velocity        uk    :  0.14981E-01 0.47013E+01
   Dimensionless distance   yplus :  0.10157E-01 0.29382E+01
   Friction thermal sca.    tstar :  0.11091E-07 0.16891E+03
   Rough dim-less th. sca.  tplus :  0.71953E-02 0.20814E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23049E+00      11   0.61033E-05   0.19345E+02 0.79715E+02 
c  Velocity[X]                                      0.74890E+01 
c  Velocity[Y]                                      0.21391E+01 
c  Velocity[Z]                                      0.97173E+01 
c  Pressure     0.23963E-04      17   0.50439E-03   0.26293E-01 0.24595E+02 
c  k            0.21983E-02      13   0.13707E-03   0.59363E-01 0.21293E+03 
c  omega        0.27924E+07       1   0.35740E-06   0.56723E+08 0.11130E+01 
c  TempK        0.83373E+04       7   0.50302E-05   0.33432E+03 0.89035E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8765e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.352          18.275       0.0025053      -0.0086702
v  Velocity[Y]             -15.526          14.258        0.057054        0.075306
v  Velocity[Z]             -25.512          18.011         -1.6522        -0.47994
v  ǁVelocityǁ         0.00030221          25.699          7.2375           6.106
v  Pressure                 -462.7          199.91          23.411          30.681
v  k                   8.1778e-012          7.7062        0.045746        0.065463
v  omega                    25.778     2.7341e+008     1.2905e+006           76356
v  TempK                    298.15          363.17          320.58          318.68
v  TurbVisc            2.0357e-019      0.00053396     1.2877e-005      3.766e-005
v  CourantNb           3.4795e-005          1.1266         0.78026         0.97362
v  FourierNb             0.0024534               1         0.38494        0.093787
v  total_pressure      1.0086e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039419     8.0249e-005      0.00021438

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.79          305.57
v  Yplus               0          2.9382         0.58991         0.43915


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.28617               2          1.1652          1.0674


 INSTANT    0.209000000E-02   TIME STEP NUMBER             209
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924209E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13676E-01 0.47054E+01
   Friction velocity        uk    :  0.13676E-01 0.47014E+01
   Dimensionless distance   yplus :  0.98132E-02 0.29383E+01
   Friction thermal sca.    tstar :  0.13214E-07 0.16820E+03
   Rough dim-less th. sca.  tplus :  0.69518E-02 0.20815E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23088E+00      11   0.60491E-05   0.19064E+02 0.79009E+02 
c  Velocity[X]                                      0.73210E+01 
c  Velocity[Y]                                      0.21438E+01 
c  Velocity[Z]                                      0.95994E+01 
c  Pressure     0.23671E-04      17   0.49738E-03   0.25947E-01 0.24581E+02 
c  k            0.22239E-02      13   0.13352E-03   0.59415E-01 0.21278E+03 
c  omega        0.27924E+07       1   0.35374E-06   0.52546E+08 0.10739E+01 
c  TempK        0.83503E+04       7   0.50096E-05   0.33119E+03 0.87680E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8754e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.355          18.283       0.0026656      -0.0086463
v  Velocity[Y]             -15.464          14.273        0.057049        0.075329
v  Velocity[Z]             -25.513          18.109         -1.6508        -0.47997
v  ǁVelocityǁ         0.00096893          25.701          7.2447          6.1141
v  Pressure                -461.63          199.98          23.473          30.689
v  k                   8.3224e-012          7.7088        0.046354        0.066104
v  omega                    26.154     2.7342e+008     1.2905e+006           76361
v  TempK                    298.15          363.17          320.66          318.78
v  TurbVisc             2.069e-019      0.00052697     1.2989e-005     3.7811e-005
v  CourantNb           3.9372e-005          1.1267         0.78041         0.97368
v  FourierNb             0.0024522               1         0.38496        0.093652
v  total_pressure      1.0086e+005     1.0152e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039251     8.0101e-005      0.00021398

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.79          305.57
v  Yplus               0          2.9383         0.59033         0.43953


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.31502               2          1.1654          1.0673


 INSTANT    0.210000000E-02   TIME STEP NUMBER             210
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924199E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15070E-01 0.47054E+01
   Friction velocity        uk    :  0.15070E-01 0.47014E+01
   Dimensionless distance   yplus :  0.10218E-01 0.29384E+01
   Friction thermal sca.    tstar :  0.15726E-07 0.16789E+03
   Rough dim-less th. sca.  tplus :  0.72383E-02 0.20816E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23127E+00      11   0.59969E-05   0.18779E+02 0.78279E+02 
c  Velocity[X]                                      0.71580E+01 
c  Velocity[Y]                                      0.21406E+01 
c  Velocity[Z]                                      0.94800E+01 
c  Pressure     0.23453E-04      18   0.49244E-03   0.25682E-01 0.24396E+02 
c  k            0.22494E-02      13   0.13035E-03   0.59369E-01 0.21248E+03 
c  omega        0.27924E+07       1   0.35049E-06   0.49599E+08 0.10411E+01 
c  TempK        0.83633E+04       7   0.49886E-05   0.32809E+03 0.86351E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      8.874e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.358          18.292        0.002825      -0.0086216
v  Velocity[Y]             -15.383          14.297        0.057046        0.075355
v  Velocity[Z]             -25.515          18.126         -1.6495           -0.48
v  ǁVelocityǁ         0.00096511          25.702          7.2518          6.1221
v  Pressure                -460.61          200.05          23.534          30.699
v  k                   8.4802e-012          7.7117        0.046962         0.06674
v  omega                    26.552     2.7342e+008     1.2905e+006           76365
v  TempK                    298.15          363.17          320.74          318.88
v  TurbVisc            2.1056e-019      0.00051887       1.31e-005     3.7958e-005
v  CourantNb           4.4536e-005          1.1269         0.78055         0.97374
v  FourierNb             0.0024514               1         0.38498        0.093513
v  total_pressure      1.0086e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039414     7.9958e-005       0.0002136

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.79          305.57
v  Yplus               0          2.9384         0.59075         0.43991


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38861               2          1.1655          1.0673


 INSTANT    0.211000000E-02   TIME STEP NUMBER             211
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924255E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15073E-01 0.47054E+01
   Friction velocity        uk    :  0.15073E-01 0.47014E+01
   Dimensionless distance   yplus :  0.10220E-01 0.29385E+01
   Friction thermal sca.    tstar :  0.18697E-07 0.16784E+03
   Rough dim-less th. sca.  tplus :  0.72398E-02 0.20816E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23166E+00      11   0.59430E-05   0.18498E+02 0.77561E+02 
c  Velocity[X]                                      0.69919E+01 
c  Velocity[Y]                                      0.21387E+01 
c  Velocity[Z]                                      0.93677E+01 
c  Pressure     0.23317E-04      17   0.48956E-03   0.25508E-01 0.24058E+02 
c  k            0.22749E-02      13   0.12668E-03   0.59288E-01 0.21223E+03 
c  omega        0.27924E+07       1   0.34760E-06   0.48667E+08 0.10277E+01 
c  TempK        0.83762E+04       7   0.49668E-05   0.32502E+03 0.85048E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8718e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.361            18.3       0.0029795      -0.0085984
v  Velocity[Y]             -15.342          14.342        0.057048        0.075389
v  Velocity[Z]             -25.517          18.142         -1.6481        -0.48003
v  ǁVelocityǁ         0.00096132          25.704          7.2589            6.13
v  Pressure                -459.64          200.11          23.593          30.706
v  k                   8.6521e-012          7.7151         0.04757        0.067371
v  omega                    26.971     2.7342e+008     1.2906e+006           76369
v  TempK                    298.15          363.17          320.81          318.97
v  TurbVisc            2.1456e-019      0.00051125     1.3209e-005     3.8101e-005
v  CourantNb           4.5515e-005          1.1272          0.7807          0.9738
v  FourierNb              0.002451               1           0.385        0.093371
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039171      7.982e-005      0.00021322

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           303.8          305.57
v  Yplus               0          2.9385         0.59117         0.44028


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50231               2          1.1657          1.0672


 INSTANT    0.212000000E-02   TIME STEP NUMBER             212
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924069E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15109E-01 0.47054E+01
   Friction velocity        uk    :  0.15109E-01 0.47014E+01
   Dimensionless distance   yplus :  0.10244E-01 0.29385E+01
   Friction thermal sca.    tstar :  0.22208E-07 0.16880E+03
   Rough dim-less th. sca.  tplus :  0.72570E-02 0.20817E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23204E+00      11   0.58879E-05   0.18217E+02 0.76844E+02 
c  Velocity[X]                                      0.68250E+01 
c  Velocity[Y]                                      0.21370E+01 
c  Velocity[Z]                                      0.92551E+01 
c  Pressure     0.23047E-04      17   0.48552E-03   0.25186E-01 0.24455E+02 
c  k            0.23003E-02      13   0.12320E-03   0.59233E-01 0.21217E+03 
c  omega        0.27924E+07       1   0.34499E-06   0.50558E+08 0.10455E+01 
c  TempK        0.83890E+04       7   0.49441E-05   0.32198E+03 0.83770E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8686e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.365          18.308       0.0031284      -0.0085812
v  Velocity[Y]             -15.339          14.453         0.05706        0.075433
v  Velocity[Z]             -25.519          18.204         -1.6467        -0.48006
v  ǁVelocityǁ         0.00088451          25.706          7.2658          6.1379
v  Pressure                -458.72          200.18          23.662          30.724
v  k                   8.8389e-012          7.7189        0.048176        0.067997
v  omega                    27.412     2.7342e+008     1.2906e+006           76373
v  TempK                    298.15          363.17          320.89          319.07
v  TurbVisc             2.189e-019      0.00052028     1.3318e-005     3.8238e-005
v  CourantNb           4.6497e-005          1.1276         0.78085         0.97385
v  FourierNb              0.002451               1         0.38502        0.093224
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.003971     7.9688e-005      0.00021286

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           303.8          305.58
v  Yplus               0          2.9385         0.59159         0.44066


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4168               2          1.1659          1.0671


 INSTANT    0.213000000E-02   TIME STEP NUMBER             213
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924166E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15145E-01 0.47054E+01
   Friction velocity        uk    :  0.15144E-01 0.47013E+01
   Dimensionless distance   yplus :  0.10268E-01 0.29386E+01
   Friction thermal sca.    tstar :  0.26353E-07 0.18176E+03
   Rough dim-less th. sca.  tplus :  0.72741E-02 0.20817E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23242E+00      11   0.58435E-05   0.17936E+02 0.76134E+02 
c  Velocity[X]                                      0.66610E+01 
c  Velocity[Y]                                      0.21379E+01 
c  Velocity[Z]                                      0.91368E+01 
c  Pressure     0.22742E-04      17   0.48242E-03   0.24829E-01 0.23090E+02 
c  k            0.23256E-02      13   0.12003E-03   0.59093E-01 0.21192E+03 
c  omega        0.27924E+07       1   0.34242E-06   0.54038E+08 0.10816E+01 
c  TempK        0.84017E+04       7   0.49213E-05   0.31897E+03 0.82519E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8643e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.368          18.316       0.0032711      -0.0085677
v  Velocity[Y]              -15.41          14.383        0.057072        0.075485
v  Velocity[Z]              -25.52          18.096         -1.6453        -0.48009
v  ǁVelocityǁ         0.00095418          25.707          7.2727          6.1456
v  Pressure                -457.87          200.23          23.711          30.723
v  k                   9.0417e-012          7.7234        0.048781        0.068618
v  omega                    27.876     2.7342e+008     1.2906e+006           76377
v  TempK                    298.15          363.17          320.96          319.17
v  TurbVisc            2.2363e-019      0.00052763     1.3425e-005      3.837e-005
v  CourantNb           2.1049e-005          1.1281         0.78101         0.97392
v  FourierNb             0.0024513               1         0.38505        0.093072
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.004368     7.9559e-005      0.00021251

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           303.8          305.58
v  Yplus               0          2.9386           0.592         0.44103


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45337               2          1.1661           1.067


 INSTANT    0.214000000E-02   TIME STEP NUMBER             214
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924064E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15217E-01 0.47053E+01
   Friction velocity        uk    :  0.15217E-01 0.47013E+01
   Dimensionless distance   yplus :  0.10317E-01 0.29387E+01
   Friction thermal sca.    tstar :  0.31243E-07 0.19405E+03
   Rough dim-less th. sca.  tplus :  0.73089E-02 0.20818E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23280E+00      11   0.57867E-05   0.17656E+02 0.75396E+02 
c  Velocity[X]                                      0.64927E+01 
c  Velocity[Y]                                      0.21360E+01 
c  Velocity[Z]                                      0.90270E+01 
c  Pressure     0.22550E-04      17   0.47934E-03   0.24594E-01 0.23179E+02 
c  k            0.23508E-02      13   0.11643E-03   0.58968E-01 0.21174E+03 
c  omega        0.27924E+07       1   0.33955E-06   0.55872E+08 0.10995E+01 
c  TempK        0.84143E+04       7   0.48981E-05   0.31600E+03 0.81296E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8594e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.372          18.325       0.0034071      -0.0085608
v  Velocity[Y]             -15.443          14.332        0.057087        0.075541
v  Velocity[Z]             -25.521          18.224          -1.644        -0.48013
v  ǁVelocityǁ         0.00087828          25.709          7.2796          6.1533
v  Pressure                -457.12          200.29          23.767          30.729
v  k                   9.2617e-012          7.7287        0.049384        0.069233
v  omega                    28.365     2.7342e+008     1.2906e+006           76381
v  TempK                    298.15          363.17          321.04          319.27
v  TurbVisc            2.2876e-019      0.00052935      1.353e-005     3.8497e-005
v  CourantNb           1.1997e-005          1.1287         0.78117         0.97398
v  FourierNb              0.002452               1         0.38507        0.092914
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044561     7.9434e-005      0.00021216

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           303.8          305.58
v  Yplus               0          2.9387         0.59242         0.44141


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45693               2          1.1662          1.0669


 INSTANT    0.215000000E-02   TIME STEP NUMBER             215
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924049E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15278E-01 0.47052E+01
   Friction velocity        uk    :  0.15278E-01 0.47012E+01
   Dimensionless distance   yplus :  0.10359E-01 0.29387E+01
   Friction thermal sca.    tstar :  0.37007E-07 0.20266E+03
   Rough dim-less th. sca.  tplus :  0.73383E-02 0.20818E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23318E+00      11   0.57349E-05   0.17372E+02 0.74660E+02 
c  Velocity[X]                                      0.63253E+01 
c  Velocity[Y]                                      0.21348E+01 
c  Velocity[Z]                                      0.89122E+01 
c  Pressure     0.22197E-04      17   0.47467E-03   0.24186E-01 0.22877E+02 
c  k            0.23760E-02      13   0.11298E-03   0.58942E-01 0.21177E+03 
c  omega        0.27924E+07       1   0.33566E-06   0.49136E+08 0.10287E+01 
c  TempK        0.84269E+04       7   0.48745E-05   0.31306E+03 0.80104E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8556e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.375          18.333       0.0035359      -0.0085558
v  Velocity[Y]              -15.36           14.31        0.057103          0.0756
v  Velocity[Z]             -25.523          17.979         -1.6426        -0.48016
v  ǁVelocityǁ         0.00094771           25.71          7.2863          6.1609
v  Pressure                 -456.7          200.35          23.821          30.736
v  k                   9.4999e-012          7.7348        0.049985        0.069843
v  omega                    28.885     2.7342e+008     1.2906e+006           76385
v  TempK                    298.15          363.17          321.11          319.37
v  TurbVisc            2.3433e-019      0.00052365     1.3635e-005     3.8621e-005
v  CourantNb           2.8205e-005          1.1292         0.78132         0.97403
v  FourierNb              0.002453               1         0.38509        0.092753
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0043639     7.9314e-005      0.00021183

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.81          305.58
v  Yplus               0          2.9387         0.59283         0.44178


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55544               2          1.1664          1.0668


 INSTANT    0.216000000E-02   TIME STEP NUMBER             216
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924123E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15315E-01 0.47051E+01
   Friction velocity        uk    :  0.15315E-01 0.47011E+01
   Dimensionless distance   yplus :  0.10384E-01 0.29388E+01
   Friction thermal sca.    tstar :  0.43797E-07 0.20480E+03
   Rough dim-less th. sca.  tplus :  0.73561E-02 0.20819E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23355E+00      11   0.56824E-05   0.17089E+02 0.73914E+02 
c  Velocity[X]                                      0.61612E+01 
c  Velocity[Y]                                      0.21294E+01 
c  Velocity[Z]                                      0.87989E+01 
c  Pressure     0.21775E-04      17   0.46791E-03   0.23702E-01 0.22674E+02 
c  k            0.24011E-02      13   0.10999E-03   0.59006E-01 0.21195E+03 
c  omega        0.27924E+07       1   0.33177E-06   0.43623E+08 0.97121E+00 
c  TempK        0.84394E+04       7   0.48509E-05   0.31017E+03 0.78941E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8513e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.379          18.341       0.0036595      -0.0085515
v  Velocity[Y]             -15.304          14.313        0.057122        0.075663
v  Velocity[Z]             -25.525          18.195         -1.6412         -0.4802
v  ǁVelocityǁ         0.00094437          25.712           7.293          6.1684
v  Pressure                -456.95           200.4          23.876          30.743
v  k                   9.7578e-012          7.7419        0.050585        0.070448
v  omega                    29.438     2.7342e+008     1.2906e+006           76389
v  TempK                    298.15          363.17          321.18          319.47
v  TurbVisc            2.4035e-019      0.00051664     1.3738e-005      3.874e-005
v  CourantNb           4.9999e-005          1.1298         0.78148         0.97409
v  FourierNb             0.0024542               1         0.38511        0.092589
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0042929     7.9198e-005       0.0002115

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.81          305.59
v  Yplus               0          2.9388         0.59324         0.44216


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4039               2          1.1666          1.0667


 INSTANT    0.217000000E-02   TIME STEP NUMBER             217
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924084E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15350E-01 0.47050E+01
   Friction velocity        uk    :  0.15350E-01 0.47009E+01
   Dimensionless distance   yplus :  0.10408E-01 0.29389E+01
   Friction thermal sca.    tstar :  0.51790E-07 0.19984E+03
   Rough dim-less th. sca.  tplus :  0.73728E-02 0.20819E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23392E+00      11   0.56266E-05   0.16820E+02 0.73204E+02 
c  Velocity[X]                                      0.60012E+01 
c  Velocity[Y]                                      0.21272E+01 
c  Velocity[Z]                                      0.86918E+01 
c  Pressure     0.21587E-04      18   0.46423E-03   0.23476E-01 0.22924E+02 
c  k            0.24262E-02      13   0.10638E-03   0.59138E-01 0.21222E+03 
c  omega        0.27924E+07       1   0.32818E-06   0.42316E+08 0.95912E+00 
c  TempK        0.84518E+04       7   0.48268E-05   0.30731E+03 0.77810E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8462e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.382          18.349       0.0037806      -0.0085482
v  Velocity[Y]             -15.299          14.324        0.057144        0.075729
v  Velocity[Z]             -25.527          17.833         -1.6398        -0.48024
v  ǁVelocityǁ         0.00094131          25.714          7.2997          6.1758
v  Pressure                -457.33          200.47          23.938          30.758
v  k                   1.0037e-011          7.7502        0.051184        0.071047
v  omega                     30.03     2.7342e+008     1.2906e+006           76393
v  TempK                    298.15          363.17          321.26          319.57
v  TurbVisc            2.4688e-019      0.00050857     1.3839e-005     3.8856e-005
v  CourantNb           3.9106e-005          1.1304         0.78163         0.97415
v  FourierNb             0.0024558               1         0.38512        0.092419
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0042366     7.9084e-005      0.00021118

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.81          305.59
v  Yplus               0          2.9389         0.59365         0.44254


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42519               2          1.1668          1.0666


 INSTANT    0.218000000E-02   TIME STEP NUMBER             218
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923986E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15409E-01 0.47048E+01
   Friction velocity        uk    :  0.15409E-01 0.47008E+01
   Dimensionless distance   yplus :  0.10448E-01 0.29390E+01
   Friction thermal sca.    tstar :  0.61191E-07 0.18970E+03
   Rough dim-less th. sca.  tplus :  0.74013E-02 0.20820E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23429E+00      11   0.55768E-05   0.16559E+02 0.72507E+02 
c  Velocity[X]                                      0.58478E+01 
c  Velocity[Y]                                      0.21257E+01 
c  Velocity[Z]                                      0.85857E+01 
c  Pressure     0.21352E-04      17   0.45933E-03   0.23197E-01 0.22988E+02 
c  k            0.24513E-02      13   0.10290E-03   0.59263E-01 0.21240E+03 
c  omega        0.27924E+07       1   0.32486E-06   0.44326E+08 0.98490E+00 
c  TempK        0.84641E+04       7   0.48027E-05   0.30450E+03 0.76711E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8404e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.386          18.357       0.0039002      -0.0085458
v  Velocity[Y]             -15.363          14.342        0.057167        0.075799
v  Velocity[Z]             -25.529          18.144         -1.6384        -0.48027
v  ǁVelocityǁ         0.00093819          25.715          7.3062          6.1832
v  Pressure                -457.78          200.53          24.004          30.777
v  k                   1.0343e-011          7.7597        0.051782        0.071643
v  omega                    30.666     2.7342e+008     1.2906e+006           76397
v  TempK                    298.15          363.17          321.33          319.66
v  TurbVisc            2.5393e-019      0.00050108      1.394e-005     3.8968e-005
v  CourantNb           4.3846e-005          1.1312         0.78178          0.9742
v  FourierNb             0.0024576               1         0.38514        0.092247
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044706     7.8973e-005      0.00021086

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.82          305.59
v  Yplus               0           2.939         0.59406         0.44291


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.33346               2          1.1669          1.0664


 INSTANT    0.219000000E-02   TIME STEP NUMBER             219
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924192E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15463E-01 0.47046E+01
   Friction velocity        uk    :  0.15463E-01 0.47006E+01
   Dimensionless distance   yplus :  0.10484E-01 0.29391E+01
   Friction thermal sca.    tstar :  0.72244E-07 0.17728E+03
   Rough dim-less th. sca.  tplus :  0.74270E-02 0.20821E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23466E+00      11   0.55330E-05   0.16308E+02 0.71849E+02 
c  Velocity[X]                                      0.57008E+01 
c  Velocity[Y]                                      0.21260E+01 
c  Velocity[Z]                                      0.84808E+01 
c  Pressure     0.21156E-04      18   0.45815E-03   0.22962E-01 0.23496E+02 
c  k            0.24764E-02      13   0.99860E-04   0.59367E-01 0.21242E+03 
c  omega        0.27924E+07       1   0.32222E-06   0.50485E+08 0.10502E+01 
c  TempK        0.84764E+04       7   0.47786E-05   0.30173E+03 0.75646E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8339e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.389          18.365        0.004023      -0.0085454
v  Velocity[Y]             -15.449           14.46        0.057195        0.075874
v  Velocity[Z]              -25.53          17.668         -1.6371        -0.48031
v  ǁVelocityǁ         0.00093548          25.717          7.3127          6.1905
v  Pressure                -457.07          200.61          24.078          30.804
v  k                   1.0654e-011          7.7705         0.05238        0.072233
v  omega                    31.353     2.7342e+008     1.2906e+006           76401
v  TempK                    298.15          363.17           321.4          319.76
v  TurbVisc            2.6169e-019      0.00049922     1.4039e-005     3.9077e-005
v  CourantNb           5.2434e-005           1.132         0.78193         0.97425
v  FourierNb             0.0024598               1         0.38516         0.09207
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0049177     7.8863e-005      0.00021055

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.82          305.59
v  Yplus               0          2.9391         0.59447         0.44329


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35468               2          1.1671          1.0663


 INSTANT    0.220000000E-02   TIME STEP NUMBER             220
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924122E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15553E-01 0.47045E+01
   Friction velocity        uk    :  0.15553E-01 0.47004E+01
   Dimensionless distance   yplus :  0.10545E-01 0.29392E+01
   Friction thermal sca.    tstar :  0.85236E-07 0.16537E+03
   Rough dim-less th. sca.  tplus :  0.74703E-02 0.20821E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23503E+00      11   0.54954E-05   0.16060E+02 0.71201E+02 
c  Velocity[X]                                      0.55605E+01 
c  Velocity[Y]                                      0.21299E+01 
c  Velocity[Z]                                      0.83694E+01 
c  Pressure     0.20914E-04      18   0.45480E-03   0.22676E-01 0.22700E+02 
c  k            0.25015E-02      13   0.96414E-04   0.59420E-01 0.21227E+03 
c  omega        0.27924E+07       1   0.31882E-06   0.53243E+08 0.10825E+01 
c  TempK        0.84885E+04       7   0.47546E-05   0.29902E+03 0.74614E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8286e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.391          18.372       0.0041449       -0.008548
v  Velocity[Y]             -15.405          14.405        0.057225        0.075953
v  Velocity[Z]             -25.532          18.073         -1.6357        -0.48034
v  ǁVelocityǁ         0.00093267          25.719          7.3191          6.1977
v  Pressure                -456.84          200.67          24.145          30.825
v  k                   1.0906e-011          7.7827        0.052977        0.072819
v  omega                    32.092     2.7342e+008     1.2906e+006           76405
v  TempK                    298.15          363.17          321.48          319.86
v  TurbVisc            2.6951e-019      0.00049535     1.4137e-005     3.9183e-005
v  CourantNb           5.3137e-005          1.1327         0.78208          0.9743
v  FourierNb             0.0024623               1         0.38517        0.091892
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0054094     7.8755e-005      0.00021025

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.82           305.6
v  Yplus               0          2.9392         0.59487         0.44367


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.33179               2          1.1673          1.0662


 INSTANT    0.221000000E-02   TIME STEP NUMBER             221
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924170E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15583E-01 0.47042E+01
   Friction velocity        uk    :  0.15583E-01 0.47002E+01
   Dimensionless distance   yplus :  0.10566E-01 0.29392E+01
   Friction thermal sca.    tstar :  0.10049E-06 0.16229E+03
   Rough dim-less th. sca.  tplus :  0.74848E-02 0.20822E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23539E+00      10   0.70040E-05   0.15788E+02 0.70466E+02 
c  Velocity[X]                                      0.54203E+01 
c  Velocity[Y]                                      0.21184E+01 
c  Velocity[Z]                                      0.82497E+01 
c  Pressure     0.20598E-04      17   0.45096E-03   0.22312E-01 0.21604E+02 
c  k            0.25266E-02      13   0.93441E-04   0.59357E-01 0.21184E+03 
c  omega        0.27924E+07       1   0.31444E-06   0.43555E+08 0.98336E+00 
c  TempK        0.85006E+04       7   0.47310E-05   0.29636E+03 0.73615E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8224e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.394           18.38       0.0042701      -0.0085528
v  Velocity[Y]             -15.306           14.35        0.057257        0.076037
v  Velocity[Z]             -25.534          17.495         -1.6343        -0.48039
v  ǁVelocityǁ          0.0009299           25.72          7.3254          6.2048
v  Pressure                -457.62          200.72          24.196          30.832
v  k                   1.1178e-011          7.7964        0.053573        0.073401
v  omega                      32.7     2.7342e+008     1.2906e+006           76409
v  TempK                    298.15          363.17          321.55          319.96
v  TurbVisc            2.7587e-019      0.00048918     1.4234e-005     3.9287e-005
v  CourantNb           5.3853e-005          1.1335         0.78223         0.97435
v  FourierNb             0.0024651               1         0.38518        0.091714
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.005675      7.865e-005      0.00020995

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.82           305.6
v  Yplus               0          2.9392         0.59527         0.44405


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38298               2          1.1674          1.0661


 INSTANT    0.222000000E-02   TIME STEP NUMBER             222
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923957E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15608E-01 0.47040E+01
   Friction velocity        uk    :  0.15608E-01 0.47000E+01
   Dimensionless distance   yplus :  0.10583E-01 0.29393E+01
   Friction thermal sca.    tstar :  0.11839E-06 0.16203E+03
   Rough dim-less th. sca.  tplus :  0.74968E-02 0.20822E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23575E+00      10   0.69468E-05   0.15541E+02 0.69796E+02 
c  Velocity[X]                                      0.52853E+01 
c  Velocity[Y]                                      0.21120E+01 
c  Velocity[Z]                                      0.81436E+01 
c  Pressure     0.20355E-04      17   0.44838E-03   0.22027E-01 0.21852E+02 
c  k            0.25517E-02      13   0.90477E-04   0.59232E-01 0.21129E+03 
c  omega        0.27924E+07       1   0.31042E-06   0.38349E+08 0.92176E+00 
c  TempK        0.85126E+04       7   0.47077E-05   0.29374E+03 0.72649E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8153e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.396          18.388       0.0043943      -0.0085564
v  Velocity[Y]             -15.281          14.329        0.057292        0.076122
v  Velocity[Z]             -25.535          17.986          -1.633        -0.48043
v  ǁVelocityǁ         0.00066243          25.722          7.3316          6.2119
v  Pressure                -457.65          200.78          24.256          30.847
v  k                   1.1472e-011          7.8116        0.054168        0.073978
v  omega                    33.331     2.7342e+008     1.2906e+006           76412
v  TempK                    298.15          363.17          321.62          320.06
v  TurbVisc            2.8276e-019      0.00047812      1.433e-005     3.9389e-005
v  CourantNb           5.4557e-005          1.1344         0.78237         0.97439
v  FourierNb             0.0024683               1         0.38519        0.091535
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0057499     7.8549e-005      0.00020967

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.83           305.6
v  Yplus               0          2.9393         0.59566         0.44443


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35047               2          1.1676          1.0659


 INSTANT    0.223000000E-02   TIME STEP NUMBER             223
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924043E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15656E-01 0.47038E+01
   Friction velocity        uk    :  0.15656E-01 0.46998E+01
   Dimensionless distance   yplus :  0.10615E-01 0.29394E+01
   Friction thermal sca.    tstar :  0.13939E-06 0.16152E+03
   Rough dim-less th. sca.  tplus :  0.75200E-02 0.20823E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23611E+00      10   0.68929E-05   0.15304E+02 0.69150E+02 
c  Velocity[X]                                      0.51580E+01 
c  Velocity[Y]                                      0.21073E+01 
c  Velocity[Z]                                      0.80384E+01 
c  Pressure     0.20136E-04      18   0.44469E-03   0.21769E-01 0.21521E+02 
c  k            0.25768E-02      13   0.88075E-04   0.58983E-01 0.21047E+03 
c  omega        0.27924E+07       1   0.30703E-06   0.37340E+08 0.90816E+00 
c  TempK        0.85245E+04       7   0.46849E-05   0.29118E+03 0.71715E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.8074e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.397          18.395       0.0045183      -0.0085625
v  Velocity[Y]             -15.307          14.336        0.057328        0.076213
v  Velocity[Z]             -25.537          17.321         -1.6316        -0.48047
v  ǁVelocityǁ          0.0009246          25.724          7.3378          6.2189
v  Pressure                -457.74          200.84          24.312          30.859
v  k                   1.1789e-011          7.8283        0.054761        0.074552
v  omega                    33.983     2.7342e+008     1.2906e+006           76416
v  TempK                    298.15          363.17          321.69          320.16
v  TurbVisc             2.902e-019      0.00046569     1.4425e-005     3.9489e-005
v  CourantNb           4.3324e-005          1.1354         0.78251         0.97444
v  FourierNb             0.0024717               1          0.3852        0.091357
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0058264      7.845e-005      0.00020939

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.83           305.6
v  Yplus               0          2.9394         0.59606         0.44481


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42685               2          1.1677          1.0658


 INSTANT    0.224000000E-02   TIME STEP NUMBER             224
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923956E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15707E-01 0.47036E+01
   Friction velocity        uk    :  0.15707E-01 0.46995E+01
   Dimensionless distance   yplus :  0.10649E-01 0.29395E+01
   Friction thermal sca.    tstar :  0.16401E-06 0.16100E+03
   Rough dim-less th. sca.  tplus :  0.75440E-02 0.20824E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23646E+00      10   0.68396E-05   0.15069E+02 0.68511E+02 
c  Velocity[X]                                      0.50310E+01 
c  Velocity[Y]                                      0.21028E+01 
c  Velocity[Z]                                      0.79356E+01 
c  Pressure     0.19963E-04      17   0.44736E-03   0.21560E-01 0.21921E+02 
c  k            0.26019E-02      13   0.85567E-04   0.58697E-01 0.20970E+03 
c  omega        0.27924E+07       1   0.30487E-06   0.44630E+08 0.98573E+00 
c  TempK        0.85364E+04       7   0.46625E-05   0.28866E+03 0.70814E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7985e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.399          18.403       0.0046408      -0.0085738
v  Velocity[Y]             -15.436          14.349        0.057363        0.076305
v  Velocity[Z]              -25.54          17.893         -1.6303         -0.4805
v  ǁVelocityǁ         0.00091063          25.726          7.3439          6.2258
v  Pressure                -458.04           200.9          24.378          30.882
v  k                   1.2132e-011          7.8466        0.055352        0.075122
v  omega                    34.659     2.7342e+008     1.2906e+006           76420
v  TempK                    298.15          363.17          321.76          320.26
v  TurbVisc            2.9823e-019      0.00045203     1.4519e-005     3.9588e-005
v  CourantNb           5.5895e-005          1.1366         0.78266         0.97448
v  FourierNb             0.0024755               1         0.38521        0.091179
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0058746     7.8354e-005      0.00020912

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.83          305.61
v  Yplus               0          2.9395         0.59646         0.44519


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.2858               2          1.1679          1.0657


 INSTANT    0.225000000E-02   TIME STEP NUMBER             225
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924099E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15778E-01 0.47033E+01
   Friction velocity        uk    :  0.15778E-01 0.46993E+01
   Dimensionless distance   yplus :  0.10698E-01 0.29396E+01
   Friction thermal sca.    tstar :  0.19285E-06 0.16027E+03
   Rough dim-less th. sca.  tplus :  0.75784E-02 0.20824E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23681E+00      10   0.67948E-05   0.14841E+02 0.67883E+02 
c  Velocity[X]                                      0.49068E+01 
c  Velocity[Y]                                      0.21022E+01 
c  Velocity[Z]                                      0.78323E+01 
c  Pressure     0.19769E-04      18   0.44200E-03   0.21330E-01 0.21345E+02 
c  k            0.26270E-02      13   0.83251E-04   0.58400E-01 0.20896E+03 
c  omega        0.27924E+07       1   0.30111E-06   0.39786E+08 0.92657E+00 
c  TempK        0.85481E+04       7   0.46405E-05   0.28619E+03 0.69946E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7898e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.399           18.41       0.0047631      -0.0085845
v  Velocity[Y]             -15.417          14.386        0.057402        0.076402
v  Velocity[Z]             -25.542          17.161          -1.629        -0.48054
v  ǁVelocityǁ         0.00065743          25.728          7.3499          6.2327
v  Pressure                -458.25          200.97          24.439          30.901
v  k                   1.2501e-011          7.8663        0.055938        0.075688
v  omega                     35.36     2.7342e+008     1.2907e+006           76423
v  TempK                    298.15          363.17          321.83          320.36
v  TurbVisc            3.0689e-019      0.00043728     1.4611e-005     3.9685e-005
v  CourantNb           5.6514e-005          1.1377          0.7828         0.97452
v  FourierNb             0.0024797               1         0.38522        0.091002
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0058999      7.826e-005      0.00020885

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.84          305.61
v  Yplus               0          2.9396         0.59686         0.44557


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45289               2           1.168          1.0655


 INSTANT    0.226000000E-02   TIME STEP NUMBER             226
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924010E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15844E-01 0.47031E+01
   Friction velocity        uk    :  0.15844E-01 0.46991E+01
   Dimensionless distance   yplus :  0.10742E-01 0.29397E+01
   Friction thermal sca.    tstar :  0.22663E-06 0.15960E+03
   Rough dim-less th. sca.  tplus :  0.76099E-02 0.20825E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23716E+00      10   0.67461E-05   0.14611E+02 0.67242E+02 
c  Velocity[X]                                      0.47810E+01 
c  Velocity[Y]                                      0.20969E+01 
c  Velocity[Z]                                      0.77329E+01 
c  Pressure     0.19698E-04      18   0.44451E-03   0.21232E-01 0.21345E+02 
c  k            0.26520E-02      13   0.81034E-04   0.58057E-01 0.20817E+03 
c  omega        0.27924E+07       1   0.29837E-06   0.43043E+08 0.96199E+00 
c  TempK        0.85598E+04       7   0.46198E-05   0.28376E+03 0.69110E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7814e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -18.4          18.417       0.0048845      -0.0085961
v  Velocity[Y]             -15.358          14.489        0.057448        0.076501
v  Velocity[Z]             -25.544          17.787         -1.6276        -0.48058
v  ǁVelocityǁ         0.00091739           25.73          7.3559          6.2394
v  Pressure                -457.38          201.03            24.5           30.92
v  k                   1.2899e-011          7.8875         0.05652         0.07625
v  omega                    36.094     2.7342e+008     1.2907e+006           76427
v  TempK                    298.15          363.17          321.91          320.46
v  TurbVisc            3.1623e-019      0.00043298     1.4703e-005     3.9781e-005
v  CourantNb           5.7111e-005          1.1388         0.78295         0.97456
v  FourierNb             0.0024841               1         0.38522        0.090824
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.005915     7.8167e-005      0.00020859

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.84          305.61
v  Yplus               0          2.9397         0.59725         0.44595


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46929               2          1.1682          1.0654


 INSTANT    0.227000000E-02   TIME STEP NUMBER             227
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923991E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15876E-01 0.47028E+01
   Friction velocity        uk    :  0.15876E-01 0.46988E+01
   Dimensionless distance   yplus :  0.10764E-01 0.29398E+01
   Friction thermal sca.    tstar :  0.26618E-06 0.15927E+03
   Rough dim-less th. sca.  tplus :  0.76254E-02 0.20825E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23751E+00      10   0.67039E-05   0.14385E+02 0.66603E+02 
c  Velocity[X]                                      0.46562E+01 
c  Velocity[Y]                                      0.20929E+01 
c  Velocity[Z]                                      0.76359E+01 
c  Pressure     0.19551E-04      17   0.43474E-03   0.21054E-01 0.20546E+02 
c  k            0.26770E-02      13   0.78892E-04   0.57680E-01 0.20730E+03 
c  omega        0.27924E+07       1   0.29529E-06   0.43816E+08 0.96993E+00 
c  TempK        0.85714E+04       7   0.45994E-05   0.28139E+03 0.68309E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7723e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -18.4          18.424       0.0050042       -0.008608
v  Velocity[Y]             -15.275          14.414        0.057497        0.076602
v  Velocity[Z]             -25.546           17.13         -1.6263        -0.48062
v  ǁVelocityǁ         0.00088495          25.732          7.3617          6.2462
v  Pressure                -457.65          201.09          24.553          30.931
v  k                    1.333e-011            7.91        0.057097         0.07681
v  omega                    36.868     2.7342e+008     1.2907e+006           76430
v  TempK                    298.15          363.17          321.98          320.56
v  TurbVisc            3.2629e-019       0.0004342     1.4793e-005     3.9876e-005
v  CourantNb           5.7748e-005            1.14          0.7831          0.9746
v  FourierNb             0.0024889               1         0.38523        0.090648
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0059264     7.8076e-005      0.00020833

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.84          305.61
v  Yplus               0          2.9398         0.59763         0.44633


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42516               2          1.1683          1.0652


 INSTANT    0.228000000E-02   TIME STEP NUMBER             228
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924036E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15910E-01 0.47026E+01
   Friction velocity        uk    :  0.15910E-01 0.46985E+01
   Dimensionless distance   yplus :  0.10787E-01 0.29398E+01
   Friction thermal sca.    tstar :  0.31244E-06 0.15893E+03
   Rough dim-less th. sca.  tplus :  0.76418E-02 0.20826E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23786E+00      10   0.66556E-05   0.14157E+02 0.65945E+02 
c  Velocity[X]                                      0.45328E+01 
c  Velocity[Y]                                      0.20848E+01 
c  Velocity[Z]                                      0.75394E+01 
c  Pressure     0.19433E-04      18   0.43096E-03   0.20907E-01 0.20635E+02 
c  k            0.27019E-02      13   0.76990E-04   0.57338E-01 0.20652E+03 
c  omega        0.27924E+07       1   0.29152E-06   0.38200E+08 0.90171E+00 
c  TempK        0.85829E+04       7   0.45800E-05   0.27903E+03 0.67537E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7623e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.399          18.431       0.0051203      -0.0086253
v  Velocity[Y]             -15.249          14.358        0.057551        0.076702
v  Velocity[Z]             -25.548          17.591          -1.625        -0.48067
v  ǁVelocityǁ         0.00078778          25.734          7.3676          6.2528
v  Pressure                -457.74          201.15          24.611           30.95
v  k                   1.3797e-011          7.9338        0.057669        0.077366
v  omega                    37.689     2.7342e+008     1.2907e+006           76434
v  TempK                    298.15          363.17          322.05          320.66
v  TurbVisc             3.372e-019      0.00043413     1.4882e-005     3.9972e-005
v  CourantNb           5.8311e-005          1.1413         0.78325         0.97464
v  FourierNb             0.0024941               1         0.38523        0.090474
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0059381     7.7987e-005      0.00020807

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.84          305.61
v  Yplus               0          2.9398         0.59802         0.44671


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53586               2          1.1685          1.0651


 INSTANT    0.229000000E-02   TIME STEP NUMBER             229
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924187E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15952E-01 0.47023E+01
   Friction velocity        uk    :  0.15952E-01 0.46983E+01
   Dimensionless distance   yplus :  0.10815E-01 0.29399E+01
   Friction thermal sca.    tstar :  0.36650E-06 0.15851E+03
   Rough dim-less th. sca.  tplus :  0.76617E-02 0.20827E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23820E+00      10   0.66091E-05   0.13930E+02 0.65293E+02 
c  Velocity[X]                                      0.44138E+01 
c  Velocity[Y]                                      0.20780E+01 
c  Velocity[Z]                                      0.74385E+01 
c  Pressure     0.19166E-04      18   0.42907E-03   0.20602E-01 0.20149E+02 
c  k            0.27269E-02      13   0.74984E-04   0.57113E-01 0.20598E+03 
c  omega        0.27924E+07       1   0.28773E-06   0.34276E+08 0.85156E+00 
c  TempK        0.85944E+04       7   0.45612E-05   0.27672E+03 0.66796E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7512e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.399          18.438       0.0052332      -0.0086482
v  Velocity[Y]             -15.259          14.333        0.057608        0.076801
v  Velocity[Z]              -25.55          16.943         -1.6237        -0.48072
v  ǁVelocityǁ         0.00091053          25.736          7.3733          6.2594
v  Pressure                -457.88           201.2          24.664          30.963
v  k                   1.4301e-011          7.9588        0.058236         0.07792
v  omega                    38.565     2.7342e+008     1.2907e+006           76437
v  TempK                    298.15          363.17          322.12          320.76
v  TurbVisc            3.4902e-019      0.00043426      1.497e-005     4.0068e-005
v  CourantNb           5.8907e-005          1.1427         0.78339         0.97467
v  FourierNb             0.0024995               1         0.38524        0.090303
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0059375     7.7898e-005      0.00020782

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.85          305.62
v  Yplus               0          2.9399          0.5984         0.44709


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5082               2          1.1686           1.065


 INSTANT    0.230000000E-02   TIME STEP NUMBER             230
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924104E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16003E-01 0.47020E+01
   Friction velocity        uk    :  0.16003E-01 0.46979E+01
   Dimensionless distance   yplus :  0.10850E-01 0.29400E+01
   Friction thermal sca.    tstar :  0.42966E-06 0.15800E+03
   Rough dim-less th. sca.  tplus :  0.76864E-02 0.20827E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23855E+00      10   0.65585E-05   0.13719E+02 0.64668E+02 
c  Velocity[X]                                      0.42986E+01 
c  Velocity[Y]                                      0.20720E+01 
c  Velocity[Z]                                      0.73479E+01 
c  Pressure     0.19179E-04      20   0.42502E-03   0.20598E-01 0.20526E+02 
c  k            0.27518E-02      13   0.73007E-04   0.56958E-01 0.20555E+03 
c  omega        0.27924E+07       1   0.28485E-06   0.36937E+08 0.88814E+00 
c  TempK        0.86057E+04       7   0.45433E-05   0.27444E+03 0.66085E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7392e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.397          18.445       0.0053436      -0.0086731
v  Velocity[Y]              -15.35          14.334        0.057664        0.076901
v  Velocity[Z]             -25.552           17.49         -1.6225        -0.48077
v  ǁVelocityǁ         0.00090847          25.738           7.379           6.266
v  Pressure                -458.31          201.26          24.726          30.985
v  k                   1.4844e-011           7.985        0.058798        0.078471
v  omega                    39.512     2.7342e+008     1.2907e+006           76441
v  TempK                    298.15          363.17          322.18          320.86
v  TurbVisc            3.6177e-019      0.00043933     1.5057e-005     4.0165e-005
v  CourantNb           5.9463e-005          1.1443         0.78354          0.9747
v  FourierNb             0.0025053               1         0.38524        0.090134
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0059159     7.7811e-005      0.00020757

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.85          305.62
v  Yplus               0            2.94         0.59878         0.44747


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38574               2          1.1688          1.0648


 INSTANT    0.231000000E-02   TIME STEP NUMBER             231
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924168E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16086E-01 0.47016E+01
   Friction velocity        uk    :  0.16086E-01 0.46976E+01
   Dimensionless distance   yplus :  0.10907E-01 0.29401E+01
   Friction thermal sca.    tstar :  0.50337E-06 0.15718E+03
   Rough dim-less th. sca.  tplus :  0.77264E-02 0.20828E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23889E+00      10   0.65054E-05   0.13510E+02 0.64055E+02 
c  Velocity[X]                                      0.41836E+01 
c  Velocity[Y]                                      0.20686E+01 
c  Velocity[Z]                                      0.72575E+01 
c  Pressure     0.18975E-04      19   0.42633E-03   0.20362E-01 0.20033E+02 
c  k            0.27768E-02      13   0.71133E-04   0.56830E-01 0.20510E+03 
c  omega        0.27924E+07       1   0.28259E-06   0.47925E+08 0.10198E+01 
c  TempK        0.86171E+04       7   0.45259E-05   0.27224E+03 0.65407E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7268e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.396          18.452        0.005457      -0.0086979
v  Velocity[Y]             -15.382          14.344        0.057722        0.077005
v  Velocity[Z]             -25.554          16.827         -1.6212        -0.48082
v  ǁVelocityǁ         0.00090643           25.74          7.3846          6.2724
v  Pressure                -459.91          201.32          24.783          31.003
v  k                   1.5427e-011          8.0121        0.059357         0.07902
v  omega                    40.535     2.7342e+008     1.2907e+006           76444
v  TempK                    298.15          363.17          322.25          320.96
v  TurbVisc            3.7549e-019      0.00043894     1.5143e-005     4.0261e-005
v  CourantNb           5.9964e-005          1.1459         0.78368         0.97473
v  FourierNb             0.0025114               1         0.38525        0.089967
v  total_pressure      1.0087e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0058714     7.7726e-005      0.00020732

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.85          305.62
v  Yplus               0          2.9401         0.59916         0.44784


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40121               2          1.1689          1.0647


 INSTANT    0.232000000E-02   TIME STEP NUMBER             232
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924158E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16144E-01 0.47012E+01
   Friction velocity        uk    :  0.16144E-01 0.46972E+01
   Dimensionless distance   yplus :  0.10946E-01 0.29402E+01
   Friction thermal sca.    tstar :  0.58931E-06 0.15661E+03
   Rough dim-less th. sca.  tplus :  0.77541E-02 0.20828E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23923E+00      10   0.64505E-05   0.13300E+02 0.63438E+02 
c  Velocity[X]                                      0.40750E+01 
c  Velocity[Y]                                      0.20639E+01 
c  Velocity[Z]                                      0.71612E+01 
c  Pressure     0.18729E-04      19   0.42606E-03   0.20081E-01 0.19974E+02 
c  k            0.28017E-02      13   0.69219E-04   0.56685E-01 0.20454E+03 
c  omega        0.27924E+07       1   0.27788E-06   0.36025E+08 0.88886E+00 
c  TempK        0.86283E+04       7   0.45098E-05   0.27008E+03 0.64760E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      8.715e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.394          18.458       0.0055671      -0.0087206
v  Velocity[Y]             -15.288          14.361        0.057786        0.077112
v  Velocity[Z]             -25.557          17.406           -1.62        -0.48088
v  ǁVelocityǁ         0.00090453          25.743          7.3901          6.2789
v  Pressure                -461.78          201.38          24.842          31.023
v  k                   1.6055e-011          8.0402        0.059913        0.079568
v  omega                    41.524     2.7342e+008     1.2907e+006           76447
v  TempK                    298.15          363.17          322.32          321.06
v  TurbVisc            3.9025e-019      0.00043919     1.5228e-005     4.0358e-005
v  CourantNb           6.0473e-005          1.1474         0.78383         0.97476
v  FourierNb             0.0025177               1         0.38525        0.089805
v  total_pressure      1.0086e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.005816     7.7643e-005      0.00020708

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.86          305.63
v  Yplus               0          2.9402         0.59953         0.44821


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38491               2          1.1691          1.0646


 INSTANT    0.233000000E-02   TIME STEP NUMBER             233
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924123E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16197E-01 0.47008E+01
   Friction velocity        uk    :  0.16197E-01 0.46968E+01
   Dimensionless distance   yplus :  0.10982E-01 0.29403E+01
   Friction thermal sca.    tstar :  0.68944E-06 0.15610E+03
   Rough dim-less th. sca.  tplus :  0.77795E-02 0.20829E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23957E+00      10   0.64070E-05   0.13097E+02 0.62818E+02 
c  Velocity[X]                                      0.39733E+01 
c  Velocity[Y]                                      0.20542E+01 
c  Velocity[Z]                                      0.70693E+01 
c  Pressure     0.19003E-04      19   0.42325E-03   0.20359E-01 0.19798E+02 
c  k            0.28268E-02      13   0.67585E-04   0.56479E-01 0.20377E+03 
c  omega        0.27924E+07       1   0.27426E-06   0.33824E+08 0.86714E+00 
c  TempK        0.86395E+04       7   0.44950E-05   0.26798E+03 0.64143E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.7031e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.391          18.465       0.0056788      -0.0087479
v  Velocity[Y]             -15.236          14.406        0.057854        0.077223
v  Velocity[Z]             -25.559           16.74         -1.6188        -0.48093
v  ǁVelocityǁ         0.00090265          25.745          7.3955          6.2852
v  Pressure                -463.92          201.44            24.9          31.043
v  k                   1.6733e-011          8.0691        0.060466        0.080115
v  omega                    42.168     2.7342e+008     1.2907e+006           76451
v  TempK                    298.15          363.17          322.39          321.16
v  TurbVisc            4.0612e-019      0.00043931     1.5312e-005     4.0456e-005
v  CourantNb           6.0945e-005           1.149         0.78397         0.97479
v  FourierNb             0.0025244               1         0.38525        0.089646
v  total_pressure      1.0086e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0057516     7.7561e-005      0.00020684

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.86          305.63
v  Yplus               0          2.9403          0.5999         0.44858


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39478               2          1.1692          1.0644


 INSTANT    0.234000000E-02   TIME STEP NUMBER             234
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924085E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16231E-01 0.47004E+01
   Friction velocity        uk    :  0.16231E-01 0.46964E+01
   Dimensionless distance   yplus :  0.11005E-01 0.29403E+01
   Friction thermal sca.    tstar :  0.80596E-06 0.15576E+03
   Rough dim-less th. sca.  tplus :  0.77961E-02 0.20830E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.23990E+00      10   0.63658E-05   0.12905E+02 0.62243E+02 
c  Velocity[X]                                      0.38754E+01 
c  Velocity[Y]                                      0.20510E+01 
c  Velocity[Z]                                      0.69787E+01 
c  Pressure     0.18697E-04      18   0.42580E-03   0.20015E-01 0.19728E+02 
c  k            0.28518E-02      13   0.65814E-04   0.56219E-01 0.20286E+03 
c  omega        0.27924E+07       1   0.27132E-06   0.34858E+08 0.88848E+00 
c  TempK        0.86506E+04       7   0.44808E-05   0.26593E+03 0.63555E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.6902e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.389          18.471       0.0057904      -0.0087775
v  Velocity[Y]             -15.236          14.452        0.057929        0.077339
v  Velocity[Z]             -25.561          17.339         -1.6176        -0.48099
v  ǁVelocityǁ          0.0009007          25.747          7.4009          6.2915
v  Pressure                -466.35           201.5          24.957          31.063
v  k                   1.7472e-011          8.0985        0.061017        0.080661
v  omega                     42.84     2.7342e+008     1.2907e+006           76454
v  TempK                    298.15          363.17          322.46          321.26
v  TurbVisc            4.2329e-019      0.00043797     1.5395e-005     4.0554e-005
v  CourantNb           6.1414e-005          1.1507         0.78411         0.97482
v  FourierNb             0.0025313               1         0.38526        0.089492
v  total_pressure      1.0086e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0056794     7.7482e-005      0.00020661

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.86          305.63
v  Yplus               0          2.9403         0.60027         0.44895


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41731               2          1.1694          1.0643


 INSTANT    0.235000000E-02   TIME STEP NUMBER             235
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923993E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16275E-01 0.47000E+01
   Friction velocity        uk    :  0.16275E-01 0.46959E+01
   Dimensionless distance   yplus :  0.11035E-01 0.29404E+01
   Friction thermal sca.    tstar :  0.94142E-06 0.15534E+03
   Rough dim-less th. sca.  tplus :  0.78171E-02 0.20830E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24024E+00      10   0.63302E-05   0.12721E+02 0.61678E+02 
c  Velocity[X]                                      0.37855E+01 
c  Velocity[Y]                                      0.20454E+01 
c  Velocity[Z]                                      0.68903E+01 
c  Pressure     0.18711E-04      19   0.41801E-03   0.20014E-01 0.19990E+02 
c  k            0.28770E-02      13   0.64057E-04   0.55918E-01 0.20182E+03 
c  omega        0.27924E+07       1   0.26863E-06   0.37299E+08 0.92486E+00 
c  TempK        0.86617E+04       7   0.44673E-05   0.26394E+03 0.62994E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.6767e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.386          18.477       0.0058983       -0.008808
v  Velocity[Y]             -15.301          14.424        0.058005        0.077459
v  Velocity[Z]             -25.563          16.727         -1.6164        -0.48105
v  ǁVelocityǁ         0.00089906          25.749          7.4062          6.2977
v  Pressure                -468.92          201.56          25.021           31.09
v  k                   1.8267e-011          8.1285        0.061565        0.081207
v  omega                    43.543     2.7342e+008     1.2907e+006           76457
v  TempK                    298.15          363.17          322.53          321.36
v  TurbVisc            4.4197e-019      0.00043707     1.5478e-005     4.0654e-005
v  CourantNb           6.1896e-005          1.1525         0.78425         0.97485
v  FourierNb             0.0025385               1         0.38526        0.089342
v  total_pressure      1.0086e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0056026     7.7404e-005      0.00020638

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.87          305.63
v  Yplus               0          2.9404         0.60063         0.44932


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4084               2          1.1695          1.0642


 INSTANT    0.236000000E-02   TIME STEP NUMBER             236
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924108E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16328E-01 0.46995E+01
   Friction velocity        uk    :  0.16328E-01 0.46955E+01
   Dimensionless distance   yplus :  0.11071E-01 0.29404E+01
   Friction thermal sca.    tstar :  0.10987E-05 0.15483E+03
   Rough dim-less th. sca.  tplus :  0.78427E-02 0.20830E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24057E+00      10   0.62899E-05   0.12542E+02 0.61122E+02 
c  Velocity[X]                                      0.36974E+01 
c  Velocity[Y]                                      0.20403E+01 
c  Velocity[Z]                                      0.68045E+01 
c  Pressure     0.18617E-04      19   0.42100E-03   0.19898E-01 0.19876E+02 
c  k            0.29021E-02      13   0.62351E-04   0.55570E-01 0.20070E+03 
c  omega        0.27924E+07       1   0.26611E-06   0.40186E+08 0.96214E+00 
c  TempK        0.86726E+04       7   0.44548E-05   0.26200E+03 0.62459E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.6627e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.383          18.483       0.0060052      -0.0088388
v  Velocity[Y]             -15.384          14.355        0.058079        0.077581
v  Velocity[Z]             -25.565          17.271         -1.6152        -0.48111
v  ǁVelocityǁ         0.00089731           25.75          7.4114          6.3039
v  Pressure                -471.62          201.63          25.085          31.117
v  k                   1.9122e-011          8.1588         0.06211        0.081754
v  omega                    44.278     2.7342e+008     1.2907e+006           76460
v  TempK                    298.15          363.17          322.59          321.46
v  TurbVisc            4.6209e-019      0.00043347     1.5559e-005     4.0755e-005
v  CourantNb           6.2302e-005          1.1544         0.78439         0.97487
v  FourierNb             0.0025461               1         0.38526        0.089196
v  total_pressure      1.0085e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0055228     7.7326e-005      0.00020615

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.87          305.64
v  Yplus               0          2.9404           0.601         0.44968


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46222               2          1.1697          1.0641


 INSTANT    0.237000000E-02   TIME STEP NUMBER             237
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924210E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16406E-01 0.46990E+01
   Friction velocity        uk    :  0.16406E-01 0.46950E+01
   Dimensionless distance   yplus :  0.11124E-01 0.29405E+01
   Friction thermal sca.    tstar :  0.12812E-05 0.15409E+03
   Rough dim-less th. sca.  tplus :  0.78802E-02 0.20831E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24090E+00      10   0.62514E-05   0.12365E+02 0.60566E+02 
c  Velocity[X]                                      0.36166E+01 
c  Velocity[Y]                                      0.20355E+01 
c  Velocity[Z]                                      0.67130E+01 
c  Pressure     0.18615E-04      19   0.41605E-03   0.19880E-01 0.19798E+02 
c  k            0.29273E-02      13   0.60557E-04   0.55179E-01 0.19952E+03 
c  omega        0.27924E+07       1   0.26242E-06   0.36673E+08 0.92017E+00 
c  TempK        0.86836E+04       7   0.44436E-05   0.26009E+03 0.61947E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.6499e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.38          18.489       0.0061114      -0.0088666
v  Velocity[Y]             -15.341          14.324        0.058155        0.077703
v  Velocity[Z]             -25.566          16.676         -1.6141        -0.48117
v  ǁVelocityǁ         0.00089576          25.752          7.4165            6.31
v  Pressure                -474.39           201.7          25.148          31.144
v  k                   2.0041e-011          8.1893        0.062653        0.082301
v  omega                    45.047     2.7342e+008     1.2907e+006           76463
v  TempK                    298.15          363.17          322.66          321.56
v  TurbVisc            4.8371e-019      0.00042493      1.564e-005     4.0857e-005
v  CourantNb           6.2737e-005          1.1561         0.78453          0.9749
v  FourierNb              0.002554               1         0.38526        0.089056
v  total_pressure      1.0085e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.005441      7.725e-005      0.00020593

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.87          305.64
v  Yplus               0          2.9405         0.60135         0.45004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43793               2          1.1698           1.064


 INSTANT    0.238000000E-02   TIME STEP NUMBER             238
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924135E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16445E-01 0.46985E+01
   Friction velocity        uk    :  0.16445E-01 0.46945E+01
   Dimensionless distance   yplus :  0.11150E-01 0.29405E+01
   Friction thermal sca.    tstar :  0.14925E-05 0.15373E+03
   Rough dim-less th. sca.  tplus :  0.78988E-02 0.20831E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24123E+00      10   0.62103E-05   0.12185E+02 0.59990E+02 
c  Velocity[X]                                      0.35356E+01 
c  Velocity[Y]                                      0.20259E+01 
c  Velocity[Z]                                      0.66237E+01 
c  Pressure     0.18338E-04      19   0.41465E-03   0.19569E-01 0.19999E+02 
c  k            0.29526E-02      13   0.58840E-04   0.54776E-01 0.19835E+03 
c  omega        0.27924E+07       1   0.25887E-06   0.33203E+08 0.87384E+00 
c  TempK        0.86945E+04       7   0.44327E-05   0.25823E+03 0.61456E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.6363e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.376          18.495       0.0062206      -0.0088921
v  Velocity[Y]             -15.238          14.325        0.058232        0.077828
v  Velocity[Z]             -25.569          17.263         -1.6129        -0.48124
v  ǁVelocityǁ          0.0007582          25.754          7.4216          6.3161
v  Pressure                -477.22          201.77          25.216          31.176
v  k                   2.1028e-011          8.2199        0.063191        0.082848
v  omega                    45.854     2.7342e+008     1.2907e+006           76467
v  TempK                    298.15          363.17          322.72          321.66
v  TurbVisc            5.0696e-019      0.00042549      1.572e-005     4.0962e-005
v  CourantNb           6.3121e-005          1.1579         0.78468         0.97492
v  FourierNb              0.002562               1         0.38526        0.088921
v  total_pressure      1.0085e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0053584     7.7175e-005      0.00020571

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.87          305.64
v  Yplus               0          2.9405          0.6017          0.4504


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50057               2          1.1699          1.0638


 INSTANT    0.239000000E-02   TIME STEP NUMBER             239
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924144E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16462E-01 0.46980E+01
   Friction velocity        uk    :  0.16462E-01 0.46940E+01
   Dimensionless distance   yplus :  0.11161E-01 0.29406E+01
   Friction thermal sca.    tstar :  0.17370E-05 0.15357E+03
   Rough dim-less th. sca.  tplus :  0.79068E-02 0.20831E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24156E+00      10   0.61686E-05   0.12012E+02 0.59422E+02 
c  Velocity[X]                                      0.34568E+01 
c  Velocity[Y]                                      0.20172E+01 
c  Velocity[Z]                                      0.65381E+01 
c  Pressure     0.18153E-04      18   0.41118E-03   0.19357E-01 0.19921E+02 
c  k            0.29778E-02      13   0.57216E-04   0.54357E-01 0.19720E+03 
c  omega        0.27924E+07       1   0.25539E-06   0.28912E+08 0.81469E+00 
c  TempK        0.87053E+04       7   0.44229E-05   0.25641E+03 0.60987E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.6219e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.372          18.501       0.0063303      -0.0089184
v  Velocity[Y]              -15.21          14.339        0.058312        0.077955
v  Velocity[Z]             -25.571          16.676         -1.6118         -0.4813
v  ǁVelocityǁ         0.00089242          25.756          7.4266          6.3221
v  Pressure                -480.15          201.84          25.282          31.208
v  k                   2.2088e-011          8.2503        0.063726        0.083397
v  omega                    46.702     2.7342e+008     1.2907e+006           76470
v  TempK                    298.15          363.17          322.79          321.76
v  TurbVisc            5.3193e-019      0.00042532       1.58e-005     4.1068e-005
v  CourantNb           6.3557e-005          1.1598         0.78482         0.97495
v  FourierNb             0.0025703               1         0.38526        0.088792
v  total_pressure      1.0084e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0052764     7.7102e-005      0.00020549

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.88          305.64
v  Yplus               0          2.9406         0.60205         0.45075


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53412               2          1.1701          1.0637


 INSTANT    0.240000000E-02   TIME STEP NUMBER             240
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924011E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16479E-01 0.46975E+01
   Friction velocity        uk    :  0.16479E-01 0.46935E+01
   Dimensionless distance   yplus :  0.11173E-01 0.29407E+01
   Friction thermal sca.    tstar :  0.20195E-05 0.15340E+03
   Rough dim-less th. sca.  tplus :  0.79153E-02 0.20832E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24189E+00      10   0.61243E-05   0.11844E+02 0.58868E+02 
c  Velocity[X]                                      0.33820E+01 
c  Velocity[Y]                                      0.20091E+01 
c  Velocity[Z]                                      0.64532E+01 
c  Pressure     0.18080E-04      19   0.40820E-03   0.19263E-01 0.19881E+02 
c  k            0.30031E-02      13   0.55759E-04   0.53902E-01 0.19599E+03 
c  omega        0.27924E+07       1   0.25262E-06   0.28376E+08 0.80945E+00 
c  TempK        0.87160E+04       7   0.44137E-05   0.25463E+03 0.60538E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.6069e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.369          18.507       0.0064395      -0.0089413
v  Velocity[Y]             -15.235           14.36        0.058395        0.078089
v  Velocity[Z]             -25.573           17.29         -1.6107        -0.48137
v  ǁVelocityǁ         0.00089077          25.758          7.4315          6.3281
v  Pressure                   -483          201.91          25.349          31.241
v  k                   2.3228e-011          8.2806        0.064256        0.083946
v  omega                    47.598     2.7342e+008     1.2907e+006           76473
v  TempK                    298.15          363.17          322.86          321.86
v  TurbVisc            5.5875e-019      0.00042435     1.5878e-005     4.1175e-005
v  CourantNb           6.3957e-005          1.1619         0.78496         0.97497
v  FourierNb             0.0025788               1         0.38526        0.088668
v  total_pressure      1.0084e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0051775      7.703e-005      0.00020528

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.88          305.65
v  Yplus               0          2.9407          0.6024         0.45111


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.36042               2          1.1702          1.0636


 INSTANT    0.241000000E-02   TIME STEP NUMBER             241
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923952E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16505E-01 0.46969E+01
   Friction velocity        uk    :  0.16505E-01 0.46929E+01
   Dimensionless distance   yplus :  0.11190E-01 0.29407E+01
   Friction thermal sca.    tstar :  0.23454E-05 0.15317E+03
   Rough dim-less th. sca.  tplus :  0.79273E-02 0.20832E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24221E+00      10   0.60916E-05   0.11683E+02 0.58333E+02 
c  Velocity[X]                                      0.33073E+01 
c  Velocity[Y]                                      0.20009E+01 
c  Velocity[Z]                                      0.63745E+01 
c  Pressure     0.17909E-04      19   0.40661E-03   0.19066E-01 0.20947E+02 
c  k            0.30283E-02      13   0.54555E-04   0.53392E-01 0.19465E+03 
c  omega        0.27924E+07       1   0.25146E-06   0.36418E+08 0.91191E+00 
c  TempK        0.87266E+04       7   0.44055E-05   0.25289E+03 0.60106E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.5912e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.365          18.513       0.0065487      -0.0089629
v  Velocity[Y]             -15.328          14.427        0.058481        0.078228
v  Velocity[Z]             -25.575           16.72         -1.6097        -0.48144
v  ǁVelocityǁ         0.00088924           25.76          7.4364           6.334
v  Pressure                 -485.7          201.99           25.43          31.287
v  k                   2.4451e-011          8.3104        0.064781        0.084497
v  omega                    48.559     2.7342e+008     1.2908e+006           76476
v  TempK                    298.15          363.17          322.92          321.96
v  TurbVisc            5.8757e-019      0.00041839     1.5956e-005     4.1286e-005
v  CourantNb           6.4365e-005           1.164          0.7851           0.975
v  FourierNb             0.0025876               1         0.38526        0.088551
v  total_pressure      1.0084e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0048374      7.696e-005      0.00020507

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.88          305.65
v  Yplus               0          2.9407         0.60275         0.45146


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45809               2          1.1704          1.0635


 INSTANT    0.242000000E-02   TIME STEP NUMBER             242
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924182E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16534E-01 0.46964E+01
   Friction velocity        uk    :  0.16534E-01 0.46924E+01
   Dimensionless distance   yplus :  0.11211E-01 0.29408E+01
   Friction thermal sca.    tstar :  0.27209E-05 0.15289E+03
   Rough dim-less th. sca.  tplus :  0.79417E-02 0.20832E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24254E+00      10   0.60516E-05   0.11528E+02 0.57821E+02 
c  Velocity[X]                                      0.32348E+01 
c  Velocity[Y]                                      0.19975E+01 
c  Velocity[Z]                                      0.62957E+01 
c  Pressure     0.17864E-04      19   0.40071E-03   0.19003E-01 0.20214E+02 
c  k            0.30536E-02      13   0.53248E-04   0.52847E-01 0.19322E+03 
c  omega        0.27924E+07       1   0.24949E-06   0.41761E+08 0.97787E+00 
c  TempK        0.87373E+04       7   0.43978E-05   0.25117E+03 0.59691E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.5754e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.361          18.519       0.0066611      -0.0089842
v  Velocity[Y]             -15.394           14.44        0.058567        0.078366
v  Velocity[Z]             -25.576          17.345         -1.6087         -0.4815
v  ǁVelocityǁ         0.00088771          25.762          7.4412          6.3398
v  Pressure                -488.08          202.07          25.504          31.328
v  k                   2.5763e-011          8.3398          0.0653        0.085049
v  omega                    49.598     2.7342e+008     1.2908e+006           76479
v  TempK                    298.15          363.17          322.99          322.06
v  TurbVisc            6.1851e-019       0.0004104     1.6034e-005       4.14e-005
v  CourantNb           6.4737e-005          1.1661         0.78525         0.97502
v  FourierNb             0.0025967               1         0.38526        0.088441
v  total_pressure      1.0084e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045766     7.6891e-005      0.00020486

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.89          305.65
v  Yplus               0          2.9408         0.60309         0.45181


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40696               2          1.1705          1.0635


 INSTANT    0.243000000E-02   TIME STEP NUMBER             243
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924227E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16572E-01 0.46959E+01
   Friction velocity        uk    :  0.16572E-01 0.46919E+01
   Dimensionless distance   yplus :  0.11236E-01 0.29408E+01
   Friction thermal sca.    tstar :  0.31528E-05 0.15254E+03
   Rough dim-less th. sca.  tplus :  0.79598E-02 0.20833E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24286E+00      10   0.60366E-05   0.11370E+02 0.57268E+02 
c  Velocity[X]                                      0.31649E+01 
c  Velocity[Y]                                      0.19863E+01 
c  Velocity[Z]                                      0.62191E+01 
c  Pressure     0.17774E-04      18   0.39709E-03   0.18892E-01 0.19554E+02 
c  k            0.30788E-02      13   0.52081E-04   0.52332E-01 0.19183E+03 
c  omega        0.27924E+07       1   0.24593E-06   0.33246E+08 0.87935E+00 
c  TempK        0.87478E+04       7   0.43908E-05   0.24948E+03 0.59293E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.5606e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.357          18.524       0.0067703      -0.0090023
v  Velocity[Y]             -15.343          14.367        0.058653        0.078505
v  Velocity[Z]             -25.578          16.795         -1.6076        -0.48156
v  ǁVelocityǁ         0.00088631          25.763          7.4459          6.3456
v  Pressure                -490.24          202.14          25.572          31.363
v  k                   2.7172e-011          8.3686        0.065813        0.085603
v  omega                    50.733     2.7342e+008     1.2908e+006           76482
v  TempK                    298.15          363.17          323.05          322.16
v  TurbVisc            6.5171e-019      0.00040086     1.6112e-005     4.1517e-005
v  CourantNb           6.5106e-005          1.1681         0.78539         0.97504
v  FourierNb             0.0026061               1         0.38527        0.088337
v  total_pressure      1.0083e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045228     7.6824e-005      0.00020466

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.89          305.65
v  Yplus               0          2.9408         0.60343         0.45215


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.37722               2          1.1707          1.0634


 INSTANT    0.244000000E-02   TIME STEP NUMBER             244
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924015E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16581E-01 0.46954E+01
   Friction velocity        uk    :  0.16581E-01 0.46914E+01
   Dimensionless distance   yplus :  0.11242E-01 0.29408E+01
   Friction thermal sca.    tstar :  0.36491E-05 0.15245E+03
   Rough dim-less th. sca.  tplus :  0.79642E-02 0.20833E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24318E+00      10   0.59970E-05   0.11208E+02 0.56707E+02 
c  Velocity[X]                                      0.30915E+01 
c  Velocity[Y]                                      0.19720E+01 
c  Velocity[Z]                                      0.61447E+01 
c  Pressure     0.17627E-04      20   0.39614E-03   0.18719E-01 0.19804E+02 
c  k            0.31041E-02      13   0.51096E-04   0.51884E-01 0.19057E+03 
c  omega        0.27924E+07       1   0.24289E-06   0.33673E+08 0.87407E+00 
c  TempK        0.87583E+04       7   0.43846E-05   0.24779E+03 0.58906E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.5453e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.353           18.53       0.0068781      -0.0090162
v  Velocity[Y]             -15.236          14.345        0.058743        0.078648
v  Velocity[Z]              -25.58          17.436         -1.6066        -0.48163
v  ǁVelocityǁ         0.00088466          25.765          7.4506          6.3513
v  Pressure                -492.43          202.21          25.644          31.403
v  k                   2.8683e-011          8.3966        0.066319        0.086159
v  omega                    51.978     2.7342e+008     1.2908e+006           76485
v  TempK                    298.15          363.17          323.11          322.26
v  TurbVisc            6.8734e-019      0.00038999     1.6188e-005     4.1636e-005
v  CourantNb           6.5449e-005          1.1702         0.78554         0.97507
v  FourierNb             0.0026158               1         0.38527        0.088239
v  total_pressure      1.0083e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044753     7.6759e-005      0.00020447

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.89          305.66
v  Yplus               0          2.9408         0.60376          0.4525


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35174               2          1.1708          1.0633


 INSTANT    0.245000000E-02   TIME STEP NUMBER             245
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924112E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16585E-01 0.46949E+01
   Friction velocity        uk    :  0.16585E-01 0.46909E+01
   Dimensionless distance   yplus :  0.11245E-01 0.29408E+01
   Friction thermal sca.    tstar :  0.42186E-05 0.15242E+03
   Rough dim-less th. sca.  tplus :  0.79659E-02 0.20833E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24350E+00      10   0.59613E-05   0.11046E+02 0.56154E+02 
c  Velocity[X]                                      0.30211E+01 
c  Velocity[Y]                                      0.19593E+01 
c  Velocity[Z]                                      0.60658E+01 
c  Pressure     0.17414E-04      19   0.39244E-03   0.18479E-01 0.19783E+02 
c  k            0.31293E-02      13   0.50214E-04   0.51540E-01 0.18954E+03 
c  omega        0.27924E+07       1   0.23891E-06   0.26937E+08 0.77702E+00 
c  TempK        0.87687E+04       7   0.43788E-05   0.24612E+03 0.58531E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.5296e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.35          18.535       0.0069851      -0.0090306
v  Velocity[Y]             -15.197          14.358        0.058832        0.078794
v  Velocity[Z]             -25.582          16.902         -1.6057        -0.48169
v  ǁVelocityǁ         0.00088324          25.766          7.4552           6.357
v  Pressure                -494.24          202.29          25.718          31.446
v  k                   3.0303e-011          8.4239         0.06682        0.086717
v  omega                    53.338     2.7342e+008     1.2908e+006           76488
v  TempK                    298.15          363.17          323.18          322.36
v  TurbVisc            7.2556e-019      0.00038376     1.6264e-005     4.1758e-005
v  CourantNb           6.5853e-005          1.1724         0.78569         0.97509
v  FourierNb             0.0026258               1         0.38527        0.088147
v  total_pressure      1.0083e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.004737     7.6696e-005      0.00020428

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           303.9          305.66
v  Yplus               0          2.9408         0.60409         0.45284


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.34572               2           1.171          1.0632


 INSTANT    0.246000000E-02   TIME STEP NUMBER             246
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924006E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16583E-01 0.46944E+01
   Friction velocity        uk    :  0.16583E-01 0.46904E+01
   Dimensionless distance   yplus :  0.11244E-01 0.29409E+01
   Friction thermal sca.    tstar :  0.48707E-05 0.15243E+03
   Rough dim-less th. sca.  tplus :  0.79652E-02 0.20833E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24382E+00      10   0.59307E-05   0.10898E+02 0.55614E+02 
c  Velocity[X]                                      0.29537E+01 
c  Velocity[Y]                                      0.19486E+01 
c  Velocity[Z]                                      0.59952E+01 
c  Pressure     0.17590E-04      20   0.39634E-03   0.18650E-01 0.21150E+02 
c  k            0.31546E-02      13   0.49321E-04   0.51305E-01 0.18874E+03 
c  omega        0.27924E+07       1   0.23569E-06   0.25742E+08 0.75704E+00 
c  TempK        0.87791E+04       7   0.43733E-05   0.24445E+03 0.58169E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.5134e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.346           18.54       0.0070879      -0.0090453
v  Velocity[Y]             -15.218          14.381        0.058922        0.078947
v  Velocity[Z]             -25.583          17.558         -1.6048        -0.48176
v  ǁVelocityǁ         0.00088168          25.768          7.4598          6.3626
v  Pressure                -495.78          202.39          25.807          31.504
v  k                   3.2041e-011          8.4502        0.067316        0.087277
v  omega                    54.813     2.7341e+008     1.2908e+006           76491
v  TempK                    298.15          363.17          323.24          322.46
v  TurbVisc            7.6655e-019      0.00038484      1.634e-005     4.1884e-005
v  CourantNb           6.6192e-005          1.1746         0.78584         0.97512
v  FourierNb             0.0026363               1         0.38527        0.088062
v  total_pressure      1.0083e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0047651     7.6634e-005      0.00020409

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           303.9          305.66
v  Yplus               0          2.9409         0.60442         0.45318


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.2762               2          1.1711          1.0632


 INSTANT    0.247000000E-02   TIME STEP NUMBER             247
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924219E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16584E-01 0.46939E+01
   Friction velocity        uk    :  0.16584E-01 0.46899E+01
   Dimensionless distance   yplus :  0.11244E-01 0.29410E+01
   Friction thermal sca.    tstar :  0.56167E-05 0.15242E+03
   Rough dim-less th. sca.  tplus :  0.79657E-02 0.20834E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24414E+00      10   0.59029E-05   0.10748E+02 0.55079E+02 
c  Velocity[X]                                      0.28885E+01 
c  Velocity[Y]                                      0.19371E+01 
c  Velocity[Z]                                      0.59223E+01 
c  Pressure     0.17443E-04      19   0.39544E-03   0.18479E-01 0.20251E+02 
c  k            0.31799E-02      12   0.48201E-04   0.51134E-01 0.18805E+03 
c  omega        0.27924E+07       1   0.23289E-06   0.28181E+08 0.79005E+00 
c  TempK        0.87895E+04       7   0.43683E-05   0.24280E+03 0.57818E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.4966e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.343          18.545       0.0071904      -0.0090574
v  Velocity[Y]             -15.293          14.407        0.059011        0.079105
v  Velocity[Z]             -25.586          17.038         -1.6038        -0.48183
v  ǁVelocityǁ         0.00088039           25.77          7.4643          6.3682
v  Pressure                -497.35          202.47          25.889          31.555
v  k                   3.3899e-011          8.4755        0.067806        0.087841
v  omega                    56.408     2.7341e+008     1.2908e+006           76494
v  TempK                    298.15          363.17           323.3          322.56
v  TurbVisc            8.1052e-019      0.00038516     1.6416e-005     4.2013e-005
v  CourantNb           6.6583e-005          1.1769         0.78599         0.97514
v  FourierNb              0.002647               1         0.38528        0.087981
v  total_pressure      1.0083e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0047846     7.6573e-005      0.00020391

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           303.9          305.66
v  Yplus               0           2.941         0.60475         0.45352


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54297               2          1.1713          1.0631


 INSTANT    0.248000000E-02   TIME STEP NUMBER             248
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924244E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16595E-01 0.46934E+01
   Friction velocity        uk    :  0.16595E-01 0.46894E+01
   Dimensionless distance   yplus :  0.11252E-01 0.29410E+01
   Friction thermal sca.    tstar :  0.64689E-05 0.15232E+03
   Rough dim-less th. sca.  tplus :  0.79710E-02 0.20834E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24446E+00      10   0.58694E-05   0.10608E+02 0.54572E+02 
c  Velocity[X]                                      0.28289E+01 
c  Velocity[Y]                                      0.19262E+01 
c  Velocity[Z]                                      0.58532E+01 
c  Pressure     0.17496E-04      20   0.39515E-03   0.18519E-01 0.21100E+02 
c  k            0.32052E-02      12   0.47222E-04   0.50901E-01 0.18710E+03 
c  omega        0.27924E+07       1   0.23003E-06   0.30196E+08 0.81590E+00 
c  TempK        0.87997E+04       7   0.43639E-05   0.24117E+03 0.57479E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.4794e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.34           18.55       0.0072895      -0.0090648
v  Velocity[Y]             -15.353          14.464        0.059101        0.079274
v  Velocity[Z]             -25.588          17.712          -1.603         -0.4819
v  ǁVelocityǁ         0.00078046          25.772          7.4687          6.3737
v  Pressure                -498.98          202.57           25.98          31.615
v  k                   3.5896e-011          8.4998        0.068294        0.088408
v  omega                    57.465     2.7341e+008     1.2908e+006           76497
v  TempK                    298.15          363.17          323.36          322.65
v  TurbVisc            8.5751e-019      0.00038435      1.649e-005     4.2144e-005
v  CourantNb           6.6881e-005          1.1793         0.78613         0.97516
v  FourierNb             0.0026581               1         0.38528        0.087907
v  total_pressure      1.0083e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0047975     7.6513e-005      0.00020373

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.91          305.67
v  Yplus               0           2.941         0.60508         0.45386


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53468               2          1.1714          1.0631


 INSTANT    0.249000000E-02   TIME STEP NUMBER             249
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924298E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16607E-01 0.46930E+01
   Friction velocity        uk    :  0.16607E-01 0.46890E+01
   Dimensionless distance   yplus :  0.11260E-01 0.29411E+01
   Friction thermal sca.    tstar :  0.74408E-05 0.15221E+03
   Rough dim-less th. sca.  tplus :  0.79764E-02 0.20835E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24477E+00      10   0.58401E-05   0.10475E+02 0.54097E+02 
c  Velocity[X]                                      0.27716E+01 
c  Velocity[Y]                                      0.19198E+01 
c  Velocity[Z]                                      0.57835E+01 
c  Pressure     0.16926E-04      19   0.38911E-03   0.17900E-01 0.21052E+02 
c  k            0.32306E-02      12   0.45962E-04   0.50559E-01 0.18587E+03 
c  omega        0.27924E+07       1   0.22688E-06   0.32163E+08 0.84405E+00 
c  TempK        0.88100E+04       7   0.43600E-05   0.23955E+03 0.57150E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.4637e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.338          18.555       0.0073869      -0.0090748
v  Velocity[Y]              -15.31          14.511        0.059199        0.079456
v  Velocity[Z]             -25.589          17.206         -1.6022        -0.48197
v  ǁVelocityǁ         0.00087746          25.774          7.4731          6.3792
v  Pressure                -500.63          202.67           26.07          31.674
v  k                   3.8038e-011           8.523        0.068778        0.088979
v  omega                    57.465     2.7341e+008     1.2908e+006           76500
v  TempK                    298.15          363.17          323.43          322.75
v  TurbVisc            9.0802e-019      0.00038211     1.6565e-005     4.2278e-005
v  CourantNb           6.7281e-005          1.1815         0.78628         0.97518
v  FourierNb             0.0026695               1         0.38528        0.087838
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0048095     7.6455e-005      0.00020355

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.91          305.67
v  Yplus               0          2.9411          0.6054         0.45419


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.36401               2          1.1716           1.063


 INSTANT    0.250000000E-02   TIME STEP NUMBER             250
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924251E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16588E-01 0.46926E+01
   Friction velocity        uk    :  0.16588E-01 0.46886E+01
   Dimensionless distance   yplus :  0.11247E-01 0.29411E+01
   Friction thermal sca.    tstar :  0.85475E-05 0.15239E+03
   Rough dim-less th. sca.  tplus :  0.79673E-02 0.20835E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24509E+00      10   0.58165E-05   0.10333E+02 0.53582E+02 
c  Velocity[X]                                      0.27191E+01 
c  Velocity[Y]                                      0.19050E+01 
c  Velocity[Z]                                      0.57086E+01 
c  Pressure     0.16908E-04      19   0.38334E-03   0.17865E-01 0.20303E+02 
c  k            0.32560E-02      12   0.44948E-04   0.50147E-01 0.18444E+03 
c  omega        0.27924E+07       1   0.22303E-06   0.28862E+08 0.80294E+00 
c  TempK        0.88201E+04       7   0.43566E-05   0.23794E+03 0.56829E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.4476e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.336          18.559       0.0074805      -0.0090864
v  Velocity[Y]             -15.205          14.483        0.059301        0.079651
v  Velocity[Z]             -25.591           17.89         -1.6013        -0.48204
v  ǁVelocityǁ         0.00087593          25.775          7.4774          6.3846
v  Pressure                -502.48          202.76          26.155           31.73
v  k                   4.0335e-011          8.5452        0.069261        0.089554
v  omega                    57.465     2.7341e+008     1.2908e+006           76503
v  TempK                    298.15          363.17          323.49          322.85
v  TurbVisc             9.622e-019      0.00038076      1.664e-005     4.2417e-005
v  CourantNb           6.7602e-005          1.1838         0.78643         0.97521
v  FourierNb             0.0026813               1         0.38529        0.087776
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0049165     7.6398e-005      0.00020338

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.91          305.67
v  Yplus               0          2.9411         0.60572         0.45452


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39879               2          1.1717           1.063


 INSTANT    0.251000000E-02   TIME STEP NUMBER             251
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924223E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16554E-01 0.46922E+01
   Friction velocity        uk    :  0.16554E-01 0.46882E+01
   Dimensionless distance   yplus :  0.11224E-01 0.29411E+01
   Friction thermal sca.    tstar :  0.98059E-05 0.15269E+03
   Rough dim-less th. sca.  tplus :  0.79512E-02 0.20835E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24540E+00      10   0.57970E-05   0.10200E+02 0.53080E+02 
c  Velocity[X]                                      0.26701E+01 
c  Velocity[Y]                                      0.18915E+01 
c  Velocity[Z]                                      0.56386E+01 
c  Pressure     0.16568E-04      20   0.38893E-03   0.17491E-01 0.20728E+02 
c  k            0.32815E-02      12   0.43703E-04   0.49746E-01 0.18302E+03 
c  omega        0.27924E+07       1   0.21891E-06   0.23798E+08 0.73188E+00 
c  TempK        0.88303E+04       7   0.43533E-05   0.23634E+03 0.56515E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.4314e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.334          18.563       0.0075728      -0.0090953
v  Velocity[Y]             -15.175          14.456        0.059405        0.079857
v  Velocity[Z]             -25.593          17.383         -1.6006        -0.48211
v  ǁVelocityǁ         0.00087466          25.777          7.4816            6.39
v  Pressure                -504.37          202.86          26.244           31.79
v  k                   4.2798e-011          8.5663        0.069742        0.090133
v  omega                    57.465     2.7341e+008     1.2908e+006           76506
v  TempK                    298.15          363.17          323.55          322.95
v  TurbVisc            1.0203e-018      0.00037915     1.6714e-005     4.2559e-005
v  CourantNb           6.7997e-005           1.186         0.78657         0.97523
v  FourierNb             0.0026934               1         0.38529         0.08772
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0054082     7.6341e-005      0.00020321

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.92          305.67
v  Yplus               0          2.9411         0.60603         0.45485


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.29542               2          1.1719          1.0629


 INSTANT    0.252000000E-02   TIME STEP NUMBER             252
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924250E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16526E-01 0.46918E+01
   Friction velocity        uk    :  0.16526E-01 0.46878E+01
   Dimensionless distance   yplus :  0.11205E-01 0.29412E+01
   Friction thermal sca.    tstar :  0.11234E-04 0.15295E+03
   Rough dim-less th. sca.  tplus :  0.79377E-02 0.20836E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24571E+00      10   0.57725E-05   0.10074E+02 0.52598E+02 
c  Velocity[X]                                      0.26289E+01 
c  Velocity[Y]                                      0.18773E+01 
c  Velocity[Z]                                      0.55676E+01 
c  Pressure     0.16866E-04      20   0.38689E-03   0.17789E-01 0.20848E+02 
c  k            0.33071E-02      12   0.42450E-04   0.49375E-01 0.18166E+03 
c  omega        0.27924E+07       1   0.21513E-06   0.19971E+08 0.67136E+00 
c  TempK        0.88403E+04       7   0.43504E-05   0.23475E+03 0.56207E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.4149e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.333          18.567       0.0076639      -0.0090975
v  Velocity[Y]             -15.202          14.464        0.059512        0.080075
v  Velocity[Z]             -25.595          18.096         -1.5998        -0.48219
v  ǁVelocityǁ         0.00087323          25.779          7.4858          6.3953
v  Pressure                -506.24          202.96          26.336          31.852
v  k                   4.5437e-011          8.5864        0.070221        0.090717
v  omega                    57.466     2.7341e+008     1.2908e+006           76508
v  TempK                    298.15          363.17          323.61          323.05
v  TurbVisc            1.0826e-018      0.00037327     1.6788e-005     4.2705e-005
v  CourantNb             6.83e-005          1.1884         0.78672         0.97525
v  FourierNb             0.0027058               1         0.38529        0.087669
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0058469     7.6286e-005      0.00020305

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.92          305.68
v  Yplus               0          2.9412         0.60635         0.45518


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46826               2           1.172          1.0629


 INSTANT    0.253000000E-02   TIME STEP NUMBER             253
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924416E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16503E-01 0.46914E+01
   Friction velocity        uk    :  0.16503E-01 0.46875E+01
   Dimensionless distance   yplus :  0.11189E-01 0.29413E+01
   Friction thermal sca.    tstar :  0.12855E-04 0.15316E+03
   Rough dim-less th. sca.  tplus :  0.79267E-02 0.20836E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24603E+00      10   0.57764E-05   0.99569E+01 0.52142E+02 
c  Velocity[X]                                      0.25874E+01 
c  Velocity[Y]                                      0.18643E+01 
c  Velocity[Z]                                      0.55053E+01 
c  Pressure     0.16721E-04      20   0.39184E-03   0.17621E-01 0.19313E+02 
c  k            0.33327E-02      12   0.41169E-04   0.49027E-01 0.18038E+03 
c  omega        0.27924E+07       1   0.21290E-06   0.24065E+08 0.73060E+00 
c  TempK        0.88504E+04       7   0.43475E-05   0.23318E+03 0.55904E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.3978e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.332          18.571       0.0077531      -0.0090962
v  Velocity[Y]             -15.299          14.469        0.059616          0.0803
v  Velocity[Z]             -25.597          17.608         -1.5991        -0.48227
v  ǁVelocityǁ         0.00087196          25.781          7.4899          6.4006
v  Pressure                -508.12          203.04          26.413          31.901
v  k                   4.8264e-011          8.6055        0.070699        0.091306
v  omega                    57.466     2.7341e+008     1.2908e+006           76511
v  TempK                    298.15          363.17          323.67          323.15
v  TurbVisc            1.1494e-018      0.00036156     1.6862e-005     4.2855e-005
v  CourantNb           6.8672e-005          1.1908         0.78687         0.97527
v  FourierNb             0.0027186               1          0.3853        0.087623
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0059967     7.6231e-005      0.00020288

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.92          305.68
v  Yplus               0          2.9413         0.60667         0.45551


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43617               2          1.1722          1.0629


 INSTANT    0.254000000E-02   TIME STEP NUMBER             254
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924254E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16485E-01 0.46911E+01
   Friction velocity        uk    :  0.16484E-01 0.46871E+01
   Dimensionless distance   yplus :  0.11177E-01 0.29414E+01
   Friction thermal sca.    tstar :  0.14691E-04 0.15334E+03
   Rough dim-less th. sca.  tplus :  0.79177E-02 0.20837E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24634E+00      10   0.57768E-05   0.98453E+01 0.51714E+02 
c  Velocity[X]                                      0.25481E+01 
c  Velocity[Y]                                      0.18525E+01 
c  Velocity[Z]                                      0.54447E+01 
c  Pressure     0.16893E-04      20   0.38106E-03   0.17785E-01 0.20175E+02 
c  k            0.33584E-02      12   0.39898E-04   0.48686E-01 0.17913E+03 
c  omega        0.27924E+07       1   0.20993E-06   0.22843E+08 0.71058E+00 
c  TempK        0.88604E+04       7   0.43451E-05   0.23161E+03 0.55606E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.3809e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.331          18.574       0.0078419      -0.0090942
v  Velocity[Y]             -15.372          14.471        0.059719        0.080533
v  Velocity[Z]             -25.599          18.297         -1.5984        -0.48234
v  ǁVelocityǁ          0.0008706          25.783          7.4939          6.4058
v  Pressure                -509.94          203.13          26.499          31.958
v  k                   5.1291e-011          8.6236        0.071176        0.091901
v  omega                    57.466      2.734e+008     1.2908e+006           76514
v  TempK                    298.15          363.17          323.73          323.25
v  TurbVisc            1.2209e-018      0.00035073     1.6936e-005     4.3008e-005
v  CourantNb           6.8971e-005          1.1932         0.78701         0.97529
v  FourierNb             0.0027318               1          0.3853        0.087582
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.005613     7.6178e-005      0.00020272

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.93          305.68
v  Yplus               0          2.9414         0.60698         0.45584


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52255               2          1.1723          1.0629


 INSTANT    0.255000000E-02   TIME STEP NUMBER             255
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924296E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16464E-01 0.46908E+01
   Friction velocity        uk    :  0.16464E-01 0.46868E+01
   Dimensionless distance   yplus :  0.11163E-01 0.29414E+01
   Friction thermal sca.    tstar :  0.16766E-04 0.15353E+03
   Rough dim-less th. sca.  tplus :  0.79076E-02 0.20837E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24665E+00      10   0.57496E-05   0.97270E+01 0.51282E+02 
c  Velocity[X]                                      0.25101E+01 
c  Velocity[Y]                                      0.18404E+01 
c  Velocity[Z]                                      0.53765E+01 
c  Pressure     0.16056E-04      20   0.38043E-03   0.16889E-01 0.19777E+02 
c  k            0.33841E-02      12   0.38621E-04   0.48368E-01 0.17796E+03 
c  omega        0.27924E+07       1   0.20699E-06   0.21073E+08 0.68349E+00 
c  TempK        0.88703E+04       7   0.43427E-05   0.23007E+03 0.55312E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.3651e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.331          18.577       0.0079294      -0.0090907
v  Velocity[Y]              -15.33           14.47        0.059821        0.080774
v  Velocity[Z]             -25.601          17.744         -1.5978        -0.48242
v  ǁVelocityǁ         0.00086937          25.785          7.4979           6.411
v  Pressure                -511.76          203.22          26.582          32.013
v  k                   5.4482e-011          8.6408         0.07165        0.092501
v  omega                    57.467      2.734e+008     1.2908e+006           76517
v  TempK                    298.15          363.17          323.79          323.34
v  TurbVisc            1.2975e-018       0.0003441      1.701e-005     4.3163e-005
v  CourantNb           6.9339e-005          1.1954         0.78715         0.97531
v  FourierNb             0.0027453               1          0.3853        0.087547
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0051639     7.6126e-005      0.00020256

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.93          305.68
v  Yplus               0          2.9414         0.60729         0.45616


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35684               2          1.1725          1.0629


 INSTANT    0.256000000E-02   TIME STEP NUMBER             256
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924266E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16419E-01 0.46905E+01
   Friction velocity        uk    :  0.16419E-01 0.46865E+01
   Dimensionless distance   yplus :  0.11133E-01 0.29416E+01
   Friction thermal sca.    tstar :  0.19110E-04 0.15394E+03
   Rough dim-less th. sca.  tplus :  0.78864E-02 0.20838E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24695E+00      10   0.57134E-05   0.96165E+01 0.50859E+02 
c  Velocity[X]                                      0.24749E+01 
c  Velocity[Y]                                      0.18255E+01 
c  Velocity[Z]                                      0.53162E+01 
c  Pressure     0.16324E-04      20   0.37527E-03   0.17154E-01 0.20585E+02 
c  k            0.34100E-02      12   0.37429E-04   0.48055E-01 0.17680E+03 
c  omega        0.27924E+07       1   0.20536E-06   0.26576E+08 0.76489E+00 
c  TempK        0.88802E+04       7   0.43401E-05   0.22854E+03 0.55020E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.3492e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.331           18.58       0.0080176      -0.0090808
v  Velocity[Y]             -15.232          14.475        0.059926        0.081024
v  Velocity[Z]             -25.604          18.546         -1.5972         -0.4825
v  ǁVelocityǁ         0.00086799          25.787          7.5019          6.4161
v  Pressure                -513.58          203.32          26.673          32.077
v  k                   5.7393e-011          8.6571        0.072123        0.093107
v  omega                    57.467      2.734e+008     1.2908e+006           76520
v  TempK                    298.15          363.17          323.85          323.44
v  TurbVisc            1.3794e-018      0.00033617     1.7084e-005     4.3323e-005
v  CourantNb            6.964e-005          1.1977         0.78729         0.97533
v  FourierNb             0.0027593               1         0.38531        0.087518
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0049932     7.6077e-005      0.00020241

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.93          305.69
v  Yplus               0          2.9416          0.6076         0.45648


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45765               2          1.1726          1.0628


 INSTANT    0.257000000E-02   TIME STEP NUMBER             257
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924254E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16363E-01 0.46902E+01
   Friction velocity        uk    :  0.16363E-01 0.46862E+01
   Dimensionless distance   yplus :  0.11094E-01 0.29416E+01
   Friction thermal sca.    tstar :  0.21602E-04 0.15448E+03
   Rough dim-less th. sca.  tplus :  0.78591E-02 0.20839E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24726E+00      10   0.56897E-05   0.95113E+01 0.50456E+02 
c  Velocity[X]                                      0.24423E+01 
c  Velocity[Y]                                      0.18151E+01 
c  Velocity[Z]                                      0.52538E+01 
c  Pressure     0.15985E-04      19   0.37393E-03   0.16780E-01 0.20552E+02 
c  k            0.34358E-02      12   0.36336E-04   0.47750E-01 0.17568E+03 
c  omega        0.27924E+07       1   0.20233E-06   0.24242E+08 0.72994E+00 
c  TempK        0.88900E+04       7   0.43375E-05   0.22702E+03 0.54731E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.3332e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.331          18.583       0.0081074      -0.0090659
v  Velocity[Y]             -15.201           14.49        0.060031        0.081282
v  Velocity[Z]             -25.606          18.161         -1.5966        -0.48258
v  ǁVelocityǁ         0.00086676          25.789          7.5058          6.4211
v  Pressure                -515.29          203.42          26.764           32.14
v  k                   6.0472e-011          8.6726        0.072593        0.093719
v  omega                    57.467      2.734e+008     1.2908e+006           76522
v  TempK                    298.15          363.17           323.9          323.54
v  TurbVisc            1.4563e-018      0.00032807     1.7158e-005     4.3488e-005
v  CourantNb           7.0028e-005             1.2         0.78744         0.97535
v  FourierNb             0.0027735               1         0.38531        0.087495
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0050761     7.6028e-005      0.00020226

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.94          305.69
v  Yplus               0          2.9416          0.6079          0.4568


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38463               2          1.1728          1.0628


 INSTANT    0.258000000E-02   TIME STEP NUMBER             258
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924320E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16305E-01 0.46900E+01
   Friction velocity        uk    :  0.16305E-01 0.46860E+01
   Dimensionless distance   yplus :  0.11055E-01 0.29417E+01
   Friction thermal sca.    tstar :  0.24212E-04 0.15502E+03
   Rough dim-less th. sca.  tplus :  0.78313E-02 0.20839E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24757E+00      10   0.56536E-05   0.94073E+01 0.50033E+02 
c  Velocity[X]                                      0.24121E+01 
c  Velocity[Y]                                      0.18006E+01 
c  Velocity[Z]                                      0.51946E+01 
c  Pressure     0.16158E-04      20   0.36932E-03   0.16945E-01 0.19812E+02 
c  k            0.34618E-02      12   0.35343E-04   0.47424E-01 0.17453E+03 
c  omega        0.27924E+07       1   0.19951E-06   0.19764E+08 0.66002E+00 
c  TempK        0.88998E+04       7   0.43352E-05   0.22552E+03 0.54442E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.3169e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.331          18.586       0.0081931       -0.009048
v  Velocity[Y]             -15.228          14.427        0.060138        0.081548
v  Velocity[Z]             -25.608          18.642         -1.5961        -0.48266
v  ǁVelocityǁ         0.00086552          25.792          7.5096          6.4262
v  Pressure                -516.84          203.52          26.849          32.199
v  k                    6.373e-011          8.6873        0.073062        0.094338
v  omega                    57.468      2.734e+008     1.2908e+006           76525
v  TempK                    298.15          363.17          323.96          323.64
v  TurbVisc            1.5344e-018      0.00031813     1.7232e-005     4.3659e-005
v  CourantNb           7.0351e-005          1.2024         0.78758         0.97537
v  FourierNb             0.0027882               1         0.38532        0.087479
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0051463      7.598e-005      0.00020211

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.94          305.69
v  Yplus               0          2.9417         0.60821         0.45712


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44336               2          1.1729          1.0628


 INSTANT    0.259000000E-02   TIME STEP NUMBER             259
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924278E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16258E-01 0.46897E+01
   Friction velocity        uk    :  0.16258E-01 0.46857E+01
   Dimensionless distance   yplus :  0.11023E-01 0.29418E+01
   Friction thermal sca.    tstar :  0.27111E-04 0.15546E+03
   Rough dim-less th. sca.  tplus :  0.78090E-02 0.20840E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24787E+00      10   0.56017E-05   0.93045E+01 0.49624E+02 
c  Velocity[X]                                      0.23822E+01 
c  Velocity[Y]                                      0.17871E+01 
c  Velocity[Z]                                      0.51353E+01 
c  Pressure     0.16008E-04      20   0.36899E-03   0.16771E-01 0.20635E+02 
c  k            0.34878E-02      12   0.34450E-04   0.47048E-01 0.17325E+03 
c  omega        0.27924E+07       1   0.19758E-06   0.20961E+08 0.67790E+00 
c  TempK        0.89096E+04       7   0.43327E-05   0.22403E+03 0.54154E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.3001e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.331          18.588       0.0082765      -0.0090309
v  Velocity[Y]             -15.308          14.407        0.060244         0.08182
v  Velocity[Z]              -25.61          18.218         -1.5956        -0.48274
v  ǁVelocityǁ         0.00086438          25.794          7.5135          6.4311
v  Pressure                -518.15          203.62          26.942          32.265
v  k                   6.7177e-011          8.7013        0.073528        0.094962
v  omega                    57.468      2.734e+008     1.2908e+006           76528
v  TempK                    298.15          363.17          324.02          323.74
v  TurbVisc            1.6171e-018      0.00031081     1.7306e-005     4.3835e-005
v  CourantNb           7.0699e-005          1.2048         0.78773         0.97539
v  FourierNb             0.0028031               1         0.38532         0.08747
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0052039     7.5933e-005      0.00020197

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.95           305.7
v  Yplus               0          2.9418         0.60851         0.45744


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40152               2           1.173          1.0629


 INSTANT    0.260000000E-02   TIME STEP NUMBER             260
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924267E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16204E-01 0.46895E+01
   Friction velocity        uk    :  0.16204E-01 0.46855E+01
   Dimensionless distance   yplus :  0.10986E-01 0.29419E+01
   Friction thermal sca.    tstar :  0.30327E-04 0.15599E+03
   Rough dim-less th. sca.  tplus :  0.77829E-02 0.20841E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24818E+00      10   0.55764E-05   0.92160E+01 0.49258E+02 
c  Velocity[X]                                      0.23586E+01 
c  Velocity[Y]                                      0.17774E+01 
c  Velocity[Z]                                      0.50800E+01 
c  Pressure     0.16152E-04      19   0.36801E-03   0.16905E-01 0.21830E+02 
c  k            0.35139E-02      12   0.33546E-04   0.46631E-01 0.17186E+03 
c  omega        0.27924E+07       1   0.19582E-06   0.22251E+08 0.69529E+00 
c  TempK        0.89193E+04       7   0.43300E-05   0.22255E+03 0.53866E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.2831e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.331          18.591       0.0083574      -0.0090123
v  Velocity[Y]             -15.371          14.418        0.060347        0.082101
v  Velocity[Z]             -25.613           18.93         -1.5952        -0.48283
v  ǁVelocityǁ         0.00086319          25.796          7.5172           6.436
v  Pressure                -519.25          203.73          27.047          32.343
v  k                   7.0822e-011          8.7146        0.073991        0.095592
v  omega                    57.469      2.734e+008     1.2908e+006           76531
v  TempK                    298.15          363.17          324.08          323.83
v  TurbVisc            1.7045e-018      0.00030472      1.738e-005     4.4018e-005
v  CourantNb           7.1011e-005          1.2073         0.78787         0.97541
v  FourierNb             0.0028184               1         0.38533        0.087469
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0052524     7.5887e-005      0.00020183

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.95           305.7
v  Yplus               0          2.9419         0.60882         0.45777


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.22028               2          1.1732          1.0629


 INSTANT    0.261000000E-02   TIME STEP NUMBER             261
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924320E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16160E-01 0.46893E+01
   Friction velocity        uk    :  0.16160E-01 0.46853E+01
   Dimensionless distance   yplus :  0.10957E-01 0.29421E+01
   Friction thermal sca.    tstar :  0.33893E-04 0.15641E+03
   Rough dim-less th. sca.  tplus :  0.77618E-02 0.20842E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24848E+00      10   0.55864E-05   0.91308E+01 0.48907E+02 
c  Velocity[X]                                      0.23351E+01 
c  Velocity[Y]                                      0.17702E+01 
c  Velocity[Z]                                      0.50255E+01 
c  Pressure     0.15863E-04      20   0.36804E-03   0.16586E-01 0.20669E+02 
c  k            0.35401E-02      12   0.32833E-04   0.46167E-01 0.17036E+03 
c  omega        0.27924E+07       1   0.19371E-06   0.23075E+08 0.70916E+00 
c  TempK        0.89289E+04       7   0.43276E-05   0.22107E+03 0.53577E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.2675e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.332          18.593       0.0084349      -0.0089943
v  Velocity[Y]              -15.33          14.437        0.060451         0.08239
v  Velocity[Z]             -25.615          18.354         -1.5948        -0.48291
v  ǁVelocityǁ         0.00086211          25.799           7.521          6.4409
v  Pressure                -520.14          203.83           27.14          32.411
v  k                   7.4678e-011          8.7273        0.074451        0.096229
v  omega                    57.469     2.7339e+008     1.2909e+006           76533
v  TempK                    298.15          363.17          324.13          323.93
v  TurbVisc             1.797e-018      0.00029757     1.7455e-005     4.4207e-005
v  CourantNb           7.1369e-005          1.2096         0.78802         0.97543
v  FourierNb              0.002834               1         0.38533        0.087474
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0052917     7.5843e-005      0.00020169

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.95           305.7
v  Yplus               0          2.9421         0.60912         0.45809


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42054               2          1.1734          1.0629


 INSTANT    0.262000000E-02   TIME STEP NUMBER             262
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924348E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16083E-01 0.46892E+01
   Friction velocity        uk    :  0.16083E-01 0.46852E+01
   Dimensionless distance   yplus :  0.10905E-01 0.29422E+01
   Friction thermal sca.    tstar :  0.37840E-04 0.15715E+03
   Rough dim-less th. sca.  tplus :  0.77249E-02 0.20843E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24878E+00      10   0.55639E-05   0.90357E+01 0.48524E+02 
c  Velocity[X]                                      0.23143E+01 
c  Velocity[Y]                                      0.17569E+01 
c  Velocity[Z]                                      0.49646E+01 
c  Pressure     0.15911E-04      20   0.36510E-03   0.16618E-01 0.20801E+02 
c  k            0.35663E-02      12   0.32107E-04   0.45705E-01 0.16883E+03 
c  omega        0.27924E+07       1   0.19130E-06   0.20943E+08 0.67392E+00 
c  TempK        0.89385E+04       7   0.43250E-05   0.21961E+03 0.53287E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.2516e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.332          18.596        0.008507      -0.0089757
v  Velocity[Y]             -15.228          14.459        0.060557        0.082688
v  Velocity[Z]             -25.618          19.166         -1.5944          -0.483
v  ǁVelocityǁ           0.000861          25.802          7.5246          6.4457
v  Pressure                -520.85          203.94          27.236          32.482
v  k                   7.8756e-011          8.7395        0.074907        0.096872
v  omega                    57.469     2.7339e+008     1.2909e+006           76536
v  TempK                    298.15          363.17          324.19          324.03
v  TurbVisc            1.8949e-018      0.00028622      1.753e-005     4.4399e-005
v  CourantNb           7.1675e-005          1.2119         0.78817         0.97545
v  FourierNb             0.0028499               1         0.38534        0.087485
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0053222       7.58e-005      0.00020156

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.96           305.7
v  Yplus               0          2.9422         0.60943         0.45841


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55629               2          1.1735          1.0629


 INSTANT    0.263000000E-02   TIME STEP NUMBER             263
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924330E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15999E-01 0.46891E+01
   Friction velocity        uk    :  0.15999E-01 0.46851E+01
   Dimensionless distance   yplus :  0.10848E-01 0.29423E+01
   Friction thermal sca.    tstar :  0.42207E-04 0.15798E+03
   Rough dim-less th. sca.  tplus :  0.76845E-02 0.20844E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24908E+00      10   0.55270E-05   0.89560E+01 0.48171E+02 
c  Velocity[X]                                      0.22974E+01 
c  Velocity[Y]                                      0.17470E+01 
c  Velocity[Z]                                      0.49117E+01 
c  Pressure     0.15900E-04      20   0.36889E-03   0.16590E-01 0.21466E+02 
c  k            0.35925E-02      12   0.31456E-04   0.45266E-01 0.16736E+03 
c  omega        0.27924E+07       1   0.18899E-06   0.18450E+08 0.62920E+00 
c  TempK        0.89481E+04       7   0.43219E-05   0.21817E+03 0.52995E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.2358e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.332          18.598       0.0085771      -0.0089537
v  Velocity[Y]               -15.2          14.503        0.060665        0.082991
v  Velocity[Z]             -25.621          18.725          -1.594        -0.48309
v  ǁVelocityǁ         0.00086002          25.804          7.5283          6.4504
v  Pressure                -521.39          204.05          27.338          32.558
v  k                   8.3068e-011          8.7512         0.07536        0.097522
v  omega                     57.47     2.7339e+008     1.2909e+006           76539
v  TempK                    298.15          363.17          324.25          324.13
v  TurbVisc            1.9983e-018      0.00028279     1.7606e-005     4.4596e-005
v  CourantNb           7.2034e-005          1.2142         0.78832         0.97547
v  FourierNb             0.0028662               1         0.38534        0.087502
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.005343     7.5757e-005      0.00020143

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.96          305.71
v  Yplus               0          2.9423         0.60973         0.45873


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45691               2          1.1737           1.063


 INSTANT    0.264000000E-02   TIME STEP NUMBER             264
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924377E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15916E-01 0.46890E+01
   Friction velocity        uk    :  0.15916E-01 0.46850E+01
   Dimensionless distance   yplus :  0.10791E-01 0.29425E+01
   Friction thermal sca.    tstar :  0.47036E-04 0.15880E+03
   Rough dim-less th. sca.  tplus :  0.76447E-02 0.20845E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24938E+00      10   0.55300E-05   0.88772E+01 0.47846E+02 
c  Velocity[X]                                      0.22803E+01 
c  Velocity[Y]                                      0.17392E+01 
c  Velocity[Z]                                      0.48577E+01 
c  Pressure     0.16098E-04      20   0.36355E-03   0.16779E-01 0.21639E+02 
c  k            0.36188E-02      12   0.30809E-04   0.44872E-01 0.16599E+03 
c  omega        0.27923E+07       1   0.18771E-06   0.21282E+08 0.67432E+00 
c  TempK        0.89576E+04       7   0.43188E-05   0.21672E+03 0.52701E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.2199e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.333          18.601       0.0086435      -0.0089256
v  Velocity[Y]             -15.229          14.617        0.060779        0.083299
v  Velocity[Z]             -25.624          19.268         -1.5938        -0.48318
v  ǁVelocityǁ         0.00085894          25.807          7.5319          6.4551
v  Pressure                -521.78          204.16          27.442          32.637
v  k                   8.7627e-011          8.7625        0.075808        0.098179
v  omega                     57.47     2.7339e+008     1.2909e+006           76541
v  TempK                    298.15          363.17           324.3          324.22
v  TurbVisc            2.1077e-018      0.00028215     1.7681e-005       4.48e-005
v  CourantNb           7.2332e-005          1.2166         0.78847         0.97549
v  FourierNb             0.0028827               1         0.38535        0.087526
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0053569     7.5715e-005       0.0002013

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.96          305.71
v  Yplus               0          2.9425         0.61003         0.45904


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57325               2          1.1738           1.063


 INSTANT    0.265000000E-02   TIME STEP NUMBER             265
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924370E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15835E-01 0.46889E+01
   Friction velocity        uk    :  0.15835E-01 0.46849E+01
   Dimensionless distance   yplus :  0.10737E-01 0.29426E+01
   Friction thermal sca.    tstar :  0.52371E-04 0.15961E+03
   Rough dim-less th. sca.  tplus :  0.76059E-02 0.20846E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24968E+00      10   0.55354E-05   0.88047E+01 0.47541E+02 
c  Velocity[X]                                      0.22644E+01 
c  Velocity[Y]                                      0.17323E+01 
c  Velocity[Z]                                      0.48080E+01 
c  Pressure     0.16160E-04      19   0.36824E-03   0.16825E-01 0.21748E+02 
c  k            0.36452E-02      12   0.30187E-04   0.44544E-01 0.16475E+03 
c  omega        0.27923E+07       1   0.18696E-06   0.26567E+08 0.75152E+00 
c  TempK        0.89670E+04       7   0.43157E-05   0.21530E+03 0.52405E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.2036e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.333          18.604       0.0087041       -0.008898
v  Velocity[Y]             -15.344          14.554         0.06089        0.083608
v  Velocity[Z]             -25.626          18.738         -1.5935        -0.48328
v  ǁVelocityǁ         0.00085807           25.81          7.5354          6.4598
v  Pressure                -522.03          204.28          27.546          32.716
v  k                   9.2448e-011          8.7733        0.076252        0.098842
v  omega                    57.471     2.7339e+008     1.2909e+006           76544
v  TempK                    298.15          363.17          324.36          324.32
v  TurbVisc            2.2234e-018      0.00028145     1.7757e-005     4.5009e-005
v  CourantNb           7.2712e-005           1.219         0.78861         0.97551
v  FourierNb             0.0028996               1         0.38536        0.087556
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0053631     7.5675e-005      0.00020118

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.97          305.71
v  Yplus               0          2.9426         0.61033         0.45936


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.32622               2           1.174          1.0631


 INSTANT    0.266000000E-02   TIME STEP NUMBER             266
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924333E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15769E-01 0.46888E+01
   Friction velocity        uk    :  0.15769E-01 0.46849E+01
   Dimensionless distance   yplus :  0.10691E-01 0.29427E+01
   Friction thermal sca.    tstar :  0.58263E-04 0.16028E+03
   Rough dim-less th. sca.  tplus :  0.75739E-02 0.20847E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.24998E+00      10   0.55192E-05   0.87254E+01 0.47196E+02 
c  Velocity[X]                                      0.22470E+01 
c  Velocity[Y]                                      0.17223E+01 
c  Velocity[Z]                                      0.47561E+01 
c  Pressure     0.16177E-04      20   0.35186E-03   0.16823E-01 0.20567E+02 
c  k            0.36716E-02      12   0.29599E-04   0.44272E-01 0.16363E+03 
c  omega        0.27923E+07       1   0.18451E-06   0.24490E+08 0.72277E+00 
c  TempK        0.89764E+04       7   0.43121E-05   0.21388E+03 0.52108E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.1877e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.333          18.607       0.0087591      -0.0088715
v  Velocity[Y]             -15.394          14.513        0.061005         0.08392
v  Velocity[Z]             -25.629          19.557         -1.5933        -0.48338
v  ǁVelocityǁ         0.00085715          25.812          7.5389          6.4644
v  Pressure                -522.19          204.38          27.642          32.787
v  k                   9.7546e-011          8.7838        0.076691        0.099512
v  omega                    57.471     2.7339e+008     1.2909e+006           76547
v  TempK                    298.15          363.17          324.41          324.42
v  TurbVisc            2.3458e-018      0.00028068     1.7833e-005     4.5221e-005
v  CourantNb           7.2985e-005          1.2213         0.78876         0.97553
v  FourierNb             0.0029167               1         0.38537        0.087591
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0053696     7.5634e-005      0.00020106

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.97          305.71
v  Yplus               0          2.9427         0.61062         0.45968


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55144               2          1.1741          1.0631


 INSTANT    0.267000000E-02   TIME STEP NUMBER             267
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924305E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15691E-01 0.46888E+01
   Friction velocity        uk    :  0.15691E-01 0.46848E+01
   Dimensionless distance   yplus :  0.10639E-01 0.29429E+01
   Friction thermal sca.    tstar :  0.64763E-04 0.16108E+03
   Rough dim-less th. sca.  tplus :  0.75367E-02 0.20848E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25028E+00      10   0.55094E-05   0.86317E+01 0.46852E+02 
c  Velocity[X]                                      0.22268E+01 
c  Velocity[Y]                                      0.17132E+01 
c  Velocity[Z]                                      0.46917E+01 
c  Pressure     0.15926E-04      19   0.35678E-03   0.16544E-01 0.20331E+02 
c  k            0.36980E-02      12   0.28981E-04   0.44056E-01 0.16262E+03 
c  omega        0.27923E+07       1   0.18181E-06   0.20179E+08 0.65452E+00 
c  TempK        0.89858E+04       7   0.43086E-05   0.21248E+03 0.51810E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.1728e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.332           18.61       0.0088084      -0.0088447
v  Velocity[Y]             -15.323          14.501        0.061123        0.084236
v  Velocity[Z]             -25.632          18.998         -1.5931        -0.48348
v  ǁVelocityǁ         0.00085632          25.815          7.5424          6.4689
v  Pressure                -522.27          204.48          27.735          32.856
v  k                   1.0096e-010          8.7939        0.077127         0.10019
v  omega                    57.472     2.7339e+008     1.2909e+006           76549
v  TempK                    298.15          363.17          324.47          324.51
v  TurbVisc            2.4751e-018      0.00027983      1.791e-005     4.5439e-005
v  CourantNb           7.3322e-005          1.2236         0.78891         0.97555
v  FourierNb              0.002934               1         0.38537        0.087632
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0053733     7.5595e-005      0.00020094

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.98          305.72
v  Yplus               0          2.9429         0.61092            0.46


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44703               2          1.1743          1.0632


 INSTANT    0.268000000E-02   TIME STEP NUMBER             268
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924319E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15591E-01 0.46888E+01
   Friction velocity        uk    :  0.15591E-01 0.46848E+01
   Dimensionless distance   yplus :  0.10571E-01 0.29430E+01
   Friction thermal sca.    tstar :  0.71932E-04 0.16211E+03
   Rough dim-less th. sca.  tplus :  0.74886E-02 0.20849E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25057E+00      10   0.55289E-05   0.85520E+01 0.46519E+02 
c  Velocity[X]                                      0.22098E+01 
c  Velocity[Y]                                      0.17021E+01 
c  Velocity[Z]                                      0.46400E+01 
c  Pressure     0.16227E-04      19   0.35063E-03   0.16837E-01 0.19915E+02 
c  k            0.37246E-02      12   0.28351E-04   0.43888E-01 0.16171E+03 
c  omega        0.27923E+07       1   0.17951E-06   0.19450E+08 0.64201E+00 
c  TempK        0.89951E+04       7   0.43050E-05   0.21111E+03 0.51511E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.1578e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.332          18.614       0.0088542      -0.0088156
v  Velocity[Y]              -15.27          14.513        0.061246        0.084557
v  Velocity[Z]             -25.635          19.716         -1.5929        -0.48359
v  ǁVelocityǁ         0.00085549          25.818          7.5459          6.4735
v  Pressure                -522.29          204.58          27.826          32.923
v  k                   1.0096e-010          8.8036        0.077558         0.10087
v  omega                    57.472     2.7338e+008     1.2909e+006           76552
v  TempK                    298.15          363.17          324.52          324.61
v  TurbVisc              2.53e-018      0.00027891     1.7986e-005      4.566e-005
v  CourantNb           7.3617e-005          1.2258         0.78906         0.97557
v  FourierNb             0.0029516               1         0.38538        0.087678
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0053736     7.5558e-005      0.00020082

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.98          305.72
v  Yplus               0           2.943         0.61121         0.46031


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43073               2          1.1744          1.0632


 INSTANT    0.269000000E-02   TIME STEP NUMBER             269
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924090E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15491E-01 0.46888E+01
   Friction velocity        uk    :  0.15491E-01 0.46849E+01
   Dimensionless distance   yplus :  0.10503E-01 0.29432E+01
   Friction thermal sca.    tstar :  0.79837E-04 0.16316E+03
   Rough dim-less th. sca.  tplus :  0.74404E-02 0.20850E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25087E+00      10   0.54836E-05   0.84741E+01 0.46208E+02 
c  Velocity[X]                                      0.21950E+01 
c  Velocity[Y]                                      0.16936E+01 
c  Velocity[Z]                                      0.45854E+01 
c  Pressure     0.15390E-04      20   0.34879E-03   0.15953E-01 0.21690E+02 
c  k            0.37512E-02      12   0.27679E-04   0.43748E-01 0.16086E+03 
c  omega        0.27923E+07       1   0.17695E-06   0.15739E+08 0.57543E+00 
c  TempK        0.90044E+04       7   0.43010E-05   0.20973E+03 0.51208E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.1427e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.331          18.617       0.0089002      -0.0087883
v  Velocity[Y]             -15.259          14.529        0.061375        0.084883
v  Velocity[Z]             -25.638          19.018         -1.5927        -0.48371
v  ǁVelocityǁ         0.00085471          25.821          7.5493          6.4779
v  Pressure                -522.25          204.69          27.931          33.005
v  k                   1.0097e-010           8.813        0.077985         0.10157
v  omega                    57.473     2.7338e+008     1.2909e+006           76555
v  TempK                    298.15          363.17          324.58          324.71
v  TurbVisc              2.53e-018       0.0002779     1.8063e-005     4.5885e-005
v  CourantNb           7.3962e-005          1.2281         0.78921         0.97559
v  FourierNb             0.0029694               1         0.38539         0.08773
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0053615     7.5521e-005      0.00020071

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.98          305.72
v  Yplus               0          2.9432          0.6115         0.46063


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44432               2          1.1746          1.0633


 INSTANT    0.270000000E-02   TIME STEP NUMBER             270
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924354E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15387E-01 0.46889E+01
   Friction velocity        uk    :  0.15387E-01 0.46849E+01
   Dimensionless distance   yplus :  0.10433E-01 0.29434E+01
   Friction thermal sca.    tstar :  0.88546E-04 0.16425E+03
   Rough dim-less th. sca.  tplus :  0.73907E-02 0.20851E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25116E+00      10   0.54541E-05   0.84012E+01 0.45906E+02 
c  Velocity[X]                                      0.21811E+01 
c  Velocity[Y]                                      0.16865E+01 
c  Velocity[Z]                                      0.45337E+01 
c  Pressure     0.15520E-04      19   0.34716E-03   0.16071E-01 0.19827E+02 
c  k            0.37779E-02      12   0.26989E-04   0.43656E-01 0.16010E+03 
c  omega        0.27923E+07       1   0.17496E-06   0.15328E+08 0.56988E+00 
c  TempK        0.90136E+04       7   0.42970E-05   0.20836E+03 0.50903E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.1275e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.33          18.622       0.0089427      -0.0087569
v  Velocity[Y]             -15.281          14.548        0.061509        0.085213
v  Velocity[Z]             -25.641          19.887         -1.5926        -0.48382
v  ǁVelocityǁ           0.000854          25.824          7.5527          6.4823
v  Pressure                 -522.2          204.79          28.022          33.072
v  k                   1.0097e-010          8.8219        0.078409         0.10227
v  omega                    57.473     2.7338e+008     1.2909e+006           76557
v  TempK                    298.15          363.17          324.63           324.8
v  TurbVisc            2.5301e-018      0.00027682      1.814e-005     4.6116e-005
v  CourantNb           7.4298e-005          1.2304         0.78936         0.97561
v  FourierNb             0.0029874               1          0.3854        0.087787
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0053337     7.5485e-005       0.0002006

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.99          305.73
v  Yplus               0          2.9434         0.61179         0.46094


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.37041               2          1.1748          1.0634


 INSTANT    0.271000000E-02   TIME STEP NUMBER             271
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924269E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15293E-01 0.46889E+01
   Friction velocity        uk    :  0.15293E-01 0.46849E+01
   Dimensionless distance   yplus :  0.10369E-01 0.29435E+01
   Friction thermal sca.    tstar :  0.98141E-04 0.16527E+03
   Rough dim-less th. sca.  tplus :  0.73452E-02 0.20852E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25145E+00      10   0.54222E-05   0.83307E+01 0.45620E+02 
c  Velocity[X]                                      0.21683E+01 
c  Velocity[Y]                                      0.16802E+01 
c  Velocity[Z]                                      0.44822E+01 
c  Pressure     0.15627E-04      19   0.34511E-03   0.16167E-01 0.20456E+02 
c  k            0.38047E-02      12   0.26323E-04   0.43567E-01 0.15931E+03 
c  omega        0.27923E+07       1   0.17372E-06   0.18079E+08 0.62054E+00 
c  TempK        0.90227E+04       7   0.42929E-05   0.20699E+03 0.50595E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.1117e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.329          18.626       0.0089849      -0.0087224
v  Velocity[Y]             -15.384           14.57        0.061645         0.08555
v  Velocity[Z]             -25.644           19.47         -1.5926        -0.48394
v  ǁVelocityǁ         0.00085335          25.827           7.556          6.4867
v  Pressure                -522.12           204.9          28.117          33.144
v  k                   1.0097e-010          8.8304         0.07883         0.10297
v  omega                    57.474     2.7338e+008     1.2909e+006           76560
v  TempK                    298.15          363.17          324.69           324.9
v  TurbVisc            2.5302e-018      0.00027566     1.8218e-005     4.6353e-005
v  CourantNb            7.458e-005          1.2328         0.78951         0.97563
v  FourierNb             0.0030057               1         0.38541        0.087851
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0052909      7.545e-005      0.00020049

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          303.99          305.73
v  Yplus               0          2.9435         0.61208         0.46125


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41339               2          1.1749          1.0635


 INSTANT    0.272000000E-02   TIME STEP NUMBER             272
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924100E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15206E-01 0.46890E+01
   Friction velocity        uk    :  0.15206E-01 0.46850E+01
   Dimensionless distance   yplus :  0.10310E-01 0.29437E+01
   Friction thermal sca.    tstar :  0.10871E-03 0.16621E+03
   Rough dim-less th. sca.  tplus :  0.73035E-02 0.20854E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25175E+00      10   0.54023E-05   0.82673E+01 0.45360E+02 
c  Velocity[X]                                      0.21580E+01 
c  Velocity[Y]                                      0.16769E+01 
c  Velocity[Z]                                      0.44323E+01 
c  Pressure     0.16086E-04      20   0.34237E-03   0.16625E-01 0.21999E+02 
c  k            0.38317E-02      12   0.25784E-04   0.43485E-01 0.15850E+03 
c  omega        0.27923E+07       1   0.17413E-06   0.31307E+08 0.82134E+00 
c  TempK        0.90319E+04       7   0.42887E-05   0.20565E+03 0.50286E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.0961e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.328          18.631       0.0090236      -0.0086885
v  Velocity[Y]             -15.425          14.642        0.061788         0.08589
v  Velocity[Z]             -25.647          19.807         -1.5926        -0.48407
v  ǁVelocityǁ         0.00085271           25.83          7.5593           6.491
v  Pressure                -522.05          205.02          28.226          33.229
v  k                   1.0098e-010          8.8385        0.079248         0.10369
v  omega                    57.474     2.7338e+008     1.2909e+006           76563
v  TempK                    298.15          363.17          324.74             325
v  TurbVisc            2.5302e-018      0.00027443     1.8297e-005     4.6597e-005
v  CourantNb           7.4916e-005          1.2352         0.78966         0.97565
v  FourierNb             0.0030242               1         0.38542        0.087921
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0052333     7.5415e-005      0.00020039

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17             304          305.73
v  Yplus               0          2.9437         0.61237         0.46156


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.34731               2          1.1751          1.0636


 INSTANT    0.273000000E-02   TIME STEP NUMBER             273
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924350E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15108E-01 0.46891E+01
   Friction velocity        uk    :  0.15108E-01 0.46851E+01
   Dimensionless distance   yplus :  0.10243E-01 0.29439E+01
   Friction thermal sca.    tstar :  0.12026E-03 0.16729E+03
   Rough dim-less th. sca.  tplus :  0.72564E-02 0.20855E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25204E+00      10   0.53597E-05   0.82041E+01 0.45104E+02 
c  Velocity[X]                                      0.21475E+01 
c  Velocity[Y]                                      0.16768E+01 
c  Velocity[Z]                                      0.43798E+01 
c  Pressure     0.15649E-04      20   0.33843E-03   0.16159E-01 0.19809E+02 
c  k            0.38587E-02      12   0.25233E-04   0.43374E-01 0.15760E+03 
c  omega        0.27923E+07       1   0.17179E-06   0.30058E+08 0.80726E+00 
c  TempK        0.90409E+04       7   0.42846E-05   0.20433E+03 0.49979E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.0814e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.327          18.636       0.0090586      -0.0086541
v  Velocity[Y]             -15.335          14.653        0.061937        0.086234
v  Velocity[Z]              -25.65          19.363         -1.5926        -0.48419
v  ǁVelocityǁ         0.00085216          25.832          7.5625          6.4952
v  Pressure                   -522          205.11          28.316          33.296
v  k                   1.0098e-010           8.846        0.079663         0.10441
v  omega                    57.475     2.7338e+008     1.2909e+006           76565
v  TempK                    298.15          363.17          324.79          325.09
v  TurbVisc            2.5303e-018      0.00027313     1.8375e-005     4.6845e-005
v  CourantNb           7.5261e-005          1.2374         0.78981         0.97567
v  FourierNb              0.003043               1         0.38543        0.087997
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0051671      7.538e-005      0.00020029

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17             304          305.73
v  Yplus               0          2.9439         0.61265         0.46187


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59932               2          1.1752          1.0637


 INSTANT    0.274000000E-02   TIME STEP NUMBER             274
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924275E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14997E-01 0.46892E+01
   Friction velocity        uk    :  0.14997E-01 0.46852E+01
   Dimensionless distance   yplus :  0.10168E-01 0.29440E+01
   Friction thermal sca.    tstar :  0.13291E-03 0.16853E+03
   Rough dim-less th. sca.  tplus :  0.72032E-02 0.20855E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25232E+00      10   0.53187E-05   0.81177E+01 0.44766E+02 
c  Velocity[X]                                      0.21375E+01 
c  Velocity[Y]                                      0.16656E+01 
c  Velocity[Z]                                      0.43145E+01 
c  Pressure     0.15507E-04      19   0.33476E-03   0.15999E-01 0.19514E+02 
c  k            0.38858E-02      12   0.24654E-04   0.43229E-01 0.15662E+03 
c  omega        0.27923E+07       1   0.16743E-06   0.17003E+08 0.60450E+00 
c  TempK        0.90499E+04       7   0.42804E-05   0.20304E+03 0.49674E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.0665e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.325          18.641       0.0090893      -0.0086176
v  Velocity[Y]             -15.281          14.581         0.06209         0.08658
v  Velocity[Z]             -25.652          20.044         -1.5926        -0.48433
v  ǁVelocityǁ         0.00085164          25.835          7.5657          6.4995
v  Pressure                   -522          205.21          28.405          33.362
v  k                   1.0098e-010          8.8531        0.080077         0.10514
v  omega                    57.475     2.7338e+008     1.2909e+006           76568
v  TempK                    298.15          363.17          324.85          325.19
v  TurbVisc            2.5304e-018      0.00027176     1.8455e-005       4.71e-005
v  CourantNb           7.5551e-005          1.2397         0.78996         0.97569
v  FourierNb              0.003062               1         0.38544        0.088078
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.005102     7.5346e-005      0.00020019

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.01          305.74
v  Yplus               0           2.944         0.61292         0.46217


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60485               2          1.1754          1.0638


 INSTANT    0.275000000E-02   TIME STEP NUMBER             275
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924117E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14885E-01 0.46893E+01
   Friction velocity        uk    :  0.14885E-01 0.46853E+01
   Dimensionless distance   yplus :  0.10092E-01 0.29442E+01
   Friction thermal sca.    tstar :  0.14681E-03 0.16979E+03
   Rough dim-less th. sca.  tplus :  0.71496E-02 0.20857E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25261E+00      10   0.53040E-05   0.80456E+01 0.44475E+02 
c  Velocity[X]                                      0.21270E+01 
c  Velocity[Y]                                      0.16582E+01 
c  Velocity[Z]                                      0.42604E+01 
c  Pressure     0.15296E-04      20   0.33167E-03   0.15768E-01 0.20356E+02 
c  k            0.39131E-02      12   0.24144E-04   0.43034E-01 0.15552E+03 
c  omega        0.27923E+07       1   0.16488E-06   0.14066E+08 0.55282E+00 
c  TempK        0.90589E+04       7   0.42765E-05   0.20177E+03 0.49370E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.0516e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.324          18.646       0.0091193      -0.0085809
v  Velocity[Y]             -15.277          14.564        0.062249        0.086928
v  Velocity[Z]             -25.655          19.342         -1.5926        -0.48447
v  ǁVelocityǁ         0.00085119          25.838          7.5689          6.5036
v  Pressure                -522.03          205.31          28.501          33.436
v  k                   1.0099e-010          8.8596        0.080489         0.10588
v  omega                    57.476     2.7337e+008     1.2909e+006           76571
v  TempK                    298.15          363.17           324.9          325.28
v  TurbVisc            2.5305e-018      0.00027041     1.8535e-005     4.7362e-005
v  CourantNb           7.5849e-005           1.242         0.79011         0.97571
v  FourierNb             0.0030812               1         0.38545        0.088166
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0050456     7.5312e-005      0.00020009

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.01          305.74
v  Yplus               0          2.9442          0.6132         0.46248


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44613               2          1.1756          1.0639


 INSTANT    0.276000000E-02   TIME STEP NUMBER             276
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924386E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14775E-01 0.46894E+01
   Friction velocity        uk    :  0.14775E-01 0.46854E+01
   Dimensionless distance   yplus :  0.10018E-01 0.29443E+01
   Friction thermal sca.    tstar :  0.16207E-03 0.17106E+03
   Rough dim-less th. sca.  tplus :  0.70966E-02 0.20858E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25290E+00      10   0.53030E-05   0.79758E+01 0.44212E+02 
c  Velocity[X]                                      0.21172E+01 
c  Velocity[Y]                                      0.16532E+01 
c  Velocity[Z]                                      0.42054E+01 
c  Pressure     0.15199E-04      20   0.32627E-03   0.15655E-01 0.18910E+02 
c  k            0.39404E-02      12   0.23670E-04   0.42807E-01 0.15434E+03 
c  omega        0.27923E+07       1   0.16319E-06   0.15143E+08 0.57363E+00 
c  TempK        0.90678E+04       7   0.42722E-05   0.20053E+03 0.49067E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.0366e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.322          18.652        0.009145      -0.0085452
v  Velocity[Y]             -15.317          14.581        0.062413        0.087279
v  Velocity[Z]             -25.658          20.295         -1.5927        -0.48461
v  ǁVelocityǁ         0.00085078          25.841           7.572          6.5077
v  Pressure                -522.13           205.4          28.586          33.499
v  k                   1.0099e-010          8.8656          0.0809         0.10662
v  omega                    57.476     2.7337e+008     1.2909e+006           76573
v  TempK                    298.15          363.17          324.95          325.38
v  TurbVisc            2.5306e-018      0.00027093     1.8615e-005      4.763e-005
v  CourantNb           7.6148e-005          1.2443         0.79026         0.97573
v  FourierNb             0.0031006               1         0.38546         0.08826
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.005013     7.5278e-005          0.0002

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.02          305.74
v  Yplus               0          2.9443         0.61348         0.46278


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53577               2          1.1757           1.064


 INSTANT    0.277000000E-02   TIME STEP NUMBER             277
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924349E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14680E-01 0.46895E+01
   Friction velocity        uk    :  0.14680E-01 0.46855E+01
   Dimensionless distance   yplus :  0.99530E-02 0.29445E+01
   Friction thermal sca.    tstar :  0.17883E-03 0.17217E+03
   Rough dim-less th. sca.  tplus :  0.70508E-02 0.20859E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25318E+00      10   0.52805E-05   0.79144E+01 0.43982E+02 
c  Velocity[X]                                      0.21088E+01 
c  Velocity[Y]                                      0.16504E+01 
c  Velocity[Z]                                      0.41553E+01 
c  Pressure     0.15030E-04      19   0.32720E-03   0.15468E-01 0.19928E+02 
c  k            0.39679E-02      12   0.23260E-04   0.42571E-01 0.15313E+03 
c  omega        0.27923E+07       1   0.16234E-06   0.18859E+08 0.63922E+00 
c  TempK        0.90767E+04       7   0.42679E-05   0.19931E+03 0.48767E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.0212e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.32          18.658       0.0091675      -0.0085106
v  Velocity[Y]             -15.468          14.605        0.062575        0.087629
v  Velocity[Z]             -25.661          19.884         -1.5928        -0.48476
v  ǁVelocityǁ         0.00085042          25.843          7.5751          6.5118
v  Pressure                -522.27           205.5          28.678          33.569
v  k                   1.0099e-010          8.8709         0.08131         0.10738
v  omega                    57.477     2.7337e+008     1.2909e+006           76576
v  TempK                    298.15          363.17             325          325.47
v  TurbVisc            2.5306e-018      0.00027144     1.8696e-005     4.7902e-005
v  CourantNb            7.644e-005          1.2467         0.79041         0.97575
v  FourierNb             0.0031203               1         0.38547        0.088358
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0049987     7.5245e-005       0.0001999

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.02          305.75
v  Yplus               0          2.9445         0.61375         0.46309


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46994               2          1.1759          1.0641


 INSTANT    0.278000000E-02   TIME STEP NUMBER             278
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924214E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14591E-01 0.46896E+01
   Friction velocity        uk    :  0.14590E-01 0.46856E+01
   Dimensionless distance   yplus :  0.98926E-02 0.29446E+01
   Friction thermal sca.    tstar :  0.19722E-03 0.17322E+03
   Rough dim-less th. sca.  tplus :  0.70080E-02 0.20860E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25347E+00      10   0.52727E-05   0.78524E+01 0.43760E+02 
c  Velocity[X]                                      0.21007E+01 
c  Velocity[Y]                                      0.16512E+01 
c  Velocity[Z]                                      0.41006E+01 
c  Pressure     0.15191E-04      19   0.32719E-03   0.15621E-01 0.20260E+02 
c  k            0.39956E-02      12   0.22815E-04   0.42344E-01 0.15194E+03 
c  omega        0.27923E+07       1   0.16053E-06   0.19325E+08 0.65105E+00 
c  TempK        0.90855E+04       7   0.42633E-05   0.19812E+03 0.48471E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     8.0072e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.318          18.664       0.0091846      -0.0084757
v  Velocity[Y]             -15.389          14.628        0.062743        0.087985
v  Velocity[Z]             -25.664          20.042          -1.593        -0.48491
v  ǁVelocityǁ         0.00085014          25.846          7.5782          6.5158
v  Pressure                -522.48          205.61          28.774          33.643
v  k                     1.01e-010          8.8751        0.081719         0.10814
v  omega                    57.477     2.7337e+008     1.2909e+006           76579
v  TempK                    298.15          363.17          325.06          325.57
v  TurbVisc            2.5307e-018      0.00027191     1.8777e-005     4.8182e-005
v  CourantNb           7.6681e-005          1.2489         0.79055         0.97577
v  FourierNb             0.0031403               1         0.38548        0.088463
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0049902     7.5213e-005      0.00019981

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.03          305.75
v  Yplus               0          2.9446         0.61403          0.4634


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59598               2           1.176          1.0642


 INSTANT    0.279000000E-02   TIME STEP NUMBER             279
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924324E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14477E-01 0.46897E+01
   Friction velocity        uk    :  0.14477E-01 0.46857E+01
   Dimensionless distance   yplus :  0.98156E-02 0.29448E+01
   Friction thermal sca.    tstar :  0.21742E-03 0.17458E+03
   Rough dim-less th. sca.  tplus :  0.69534E-02 0.20861E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25375E+00      10   0.52444E-05   0.77852E+01 0.43492E+02 
c  Velocity[X]                                      0.20930E+01 
c  Velocity[Y]                                      0.16439E+01 
c  Velocity[Z]                                      0.40484E+01 
c  Pressure     0.15064E-04      19   0.32177E-03   0.15480E-01 0.18445E+02 
c  k            0.40234E-02      12   0.22377E-04   0.42119E-01 0.15074E+03 
c  omega        0.27923E+07       1   0.15825E-06   0.16749E+08 0.60918E+00 
c  TempK        0.90943E+04       7   0.42586E-05   0.19696E+03 0.48178E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.9931e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.316           18.67       0.0091969      -0.0084396
v  Velocity[Y]             -15.312           14.65        0.062915        0.088343
v  Velocity[Z]             -25.667          19.699         -1.5931        -0.48506
v  ǁVelocityǁ         0.00084986          25.849          7.5812          6.5198
v  Pressure                -522.74           205.7          28.854          33.702
v  k                     1.01e-010          8.8782        0.082128         0.10891
v  omega                    57.478     2.7337e+008     1.2909e+006           76581
v  TempK                    298.15          363.17          325.11          325.66
v  TurbVisc            2.5308e-018      0.00027236     1.8859e-005     4.8467e-005
v  CourantNb           7.7029e-005          1.2511          0.7907         0.97579
v  FourierNb             0.0031606               1         0.38549        0.088572
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0049811      7.518e-005      0.00019972

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.03          305.75
v  Yplus               0          2.9448         0.61431          0.4637


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41237               2          1.1762          1.0644


 INSTANT    0.280000000E-02   TIME STEP NUMBER             280
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924200E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14370E-01 0.46898E+01
   Friction velocity        uk    :  0.14370E-01 0.46858E+01
   Dimensionless distance   yplus :  0.97432E-02 0.29450E+01
   Friction thermal sca.    tstar :  0.23957E-03 0.17587E+03
   Rough dim-less th. sca.  tplus :  0.69022E-02 0.20862E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25403E+00      10   0.52402E-05   0.77245E+01 0.43259E+02 
c  Velocity[X]                                      0.20870E+01 
c  Velocity[Y]                                      0.16403E+01 
c  Velocity[Z]                                      0.39972E+01 
c  Pressure     0.15441E-04      20   0.31782E-03   0.15856E-01 0.19265E+02 
c  k            0.40513E-02      12   0.21962E-04   0.41900E-01 0.14956E+03 
c  omega        0.27923E+07       1   0.15613E-06   0.14178E+08 0.56284E+00 
c  TempK        0.91030E+04       7   0.42538E-05   0.19582E+03 0.47887E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.9787e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.314          18.676       0.0092059      -0.0084032
v  Velocity[Y]             -15.286          14.689        0.063093        0.088705
v  Velocity[Z]              -25.67          20.214         -1.5933        -0.48522
v  ǁVelocityǁ         0.00067654          25.852          7.5842          6.5237
v  Pressure                -523.06           205.8          28.942          33.768
v  k                     1.01e-010          8.8802        0.082535         0.10969
v  omega                    57.478     2.7337e+008     1.2909e+006           76584
v  TempK                    298.15          363.17          325.16          325.76
v  TurbVisc            2.5309e-018      0.00027278     1.8942e-005     4.8759e-005
v  CourantNb           7.7281e-005          1.2533         0.79084         0.97581
v  FourierNb             0.0031813               1          0.3855        0.088689
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0052238      7.515e-005      0.00019964

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.03          305.75
v  Yplus               0           2.945         0.61458         0.46401


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.486               2          1.1763          1.0645


 INSTANT    0.281000000E-02   TIME STEP NUMBER             281
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924408E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14261E-01 0.46899E+01
   Friction velocity        uk    :  0.14261E-01 0.46859E+01
   Dimensionless distance   yplus :  0.96689E-02 0.29451E+01
   Friction thermal sca.    tstar :  0.26387E-03 0.17723E+03
   Rough dim-less th. sca.  tplus :  0.68495E-02 0.20864E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25431E+00      10   0.52144E-05   0.76631E+01 0.43051E+02 
c  Velocity[X]                                      0.20814E+01 
c  Velocity[Y]                                      0.16394E+01 
c  Velocity[Z]                                      0.39423E+01 
c  Pressure     0.14815E-04      19   0.31649E-03   0.15204E-01 0.18761E+02 
c  k            0.40793E-02      12   0.21554E-04   0.41724E-01 0.14850E+03 
c  omega        0.27923E+07       1   0.15545E-06   0.17457E+08 0.62267E+00 
c  TempK        0.91117E+04       7   0.42490E-05   0.19470E+03 0.47598E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      7.964e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.312          18.682       0.0092119      -0.0083675
v  Velocity[Y]             -15.303          14.797         0.06328         0.08907
v  Velocity[Z]             -25.672          19.627         -1.5935        -0.48539
v  ǁVelocityǁ         0.00084949          25.855          7.5872          6.5276
v  Pressure                -523.41          205.88          29.026           33.83
v  k                   1.0101e-010          8.8813        0.082942         0.11047
v  omega                    57.479     2.7337e+008     1.2909e+006           76587
v  TempK                    298.15          363.17          325.21          325.85
v  TurbVisc             2.531e-018      0.00027318     1.9025e-005     4.9057e-005
v  CourantNb            7.763e-005          1.2557         0.79098         0.97583
v  FourierNb             0.0032021               1         0.38551         0.08881
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0054317     7.5119e-005      0.00019955

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.04          305.76
v  Yplus               0          2.9451         0.61485         0.46432


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48024               2          1.1765          1.0646


 INSTANT    0.282000000E-02   TIME STEP NUMBER             282
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924189E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14168E-01 0.46901E+01
   Friction velocity        uk    :  0.14168E-01 0.46861E+01
   Dimensionless distance   yplus :  0.96059E-02 0.29452E+01
   Friction thermal sca.    tstar :  0.29054E-03 0.17839E+03
   Rough dim-less th. sca.  tplus :  0.68049E-02 0.20864E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25459E+00      10   0.52102E-05   0.76060E+01 0.42848E+02 
c  Velocity[X]                                      0.20781E+01 
c  Velocity[Y]                                      0.16400E+01 
c  Velocity[Z]                                      0.38879E+01 
c  Pressure     0.15144E-04      19   0.31431E-03   0.15532E-01 0.19174E+02 
c  k            0.41074E-02      12   0.21338E-04   0.41571E-01 0.14752E+03 
c  omega        0.27923E+07       1   0.15473E-06   0.20402E+08 0.67456E+00 
c  TempK        0.91203E+04       7   0.42443E-05   0.19363E+03 0.47314E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.9489e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.31          18.688       0.0092103      -0.0083321
v  Velocity[Y]             -15.372          14.721         0.06347        0.089439
v  Velocity[Z]             -25.675            20.4         -1.5938        -0.48557
v  ǁVelocityǁ         0.00084947          25.857          7.5901          6.5314
v  Pressure                -523.81          205.98          29.114          33.897
v  k                   1.0101e-010          8.8816        0.083348         0.11127
v  omega                    57.479     2.7336e+008     1.2909e+006           76589
v  TempK                    298.15          363.17          325.26          325.95
v  TurbVisc            2.5311e-018      0.00027211     1.9108e-005      4.936e-005
v  CourantNb           7.7893e-005           1.258         0.79112         0.97584
v  FourierNb             0.0032232               1         0.38553        0.088936
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0054667     7.5089e-005      0.00019947

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.04          305.76
v  Yplus               0          2.9452         0.61513         0.46463


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50433               2          1.1766          1.0648


 INSTANT    0.283000000E-02   TIME STEP NUMBER             283
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924252E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14075E-01 0.46902E+01
   Friction velocity        uk    :  0.14075E-01 0.46862E+01
   Dimensionless distance   yplus :  0.95434E-02 0.29454E+01
   Friction thermal sca.    tstar :  0.31980E-03 0.17956E+03
   Rough dim-less th. sca.  tplus :  0.67606E-02 0.20865E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25487E+00      10   0.51882E-05   0.75457E+01 0.42611E+02 
c  Velocity[X]                                      0.20726E+01 
c  Velocity[Y]                                      0.16373E+01 
c  Velocity[Z]                                      0.38358E+01 
c  Pressure     0.14632E-04      19   0.31169E-03   0.14999E-01 0.18790E+02 
c  k            0.41357E-02      12   0.21052E-04   0.41353E-01 0.14638E+03 
c  omega        0.27923E+07       1   0.15392E-06   0.21313E+08 0.69394E+00 
c  TempK        0.91289E+04       7   0.42395E-05   0.19257E+03 0.47036E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.9337e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.308          18.695       0.0092069      -0.0082964
v  Velocity[Y]             -15.435          14.671        0.063662        0.089809
v  Velocity[Z]             -25.678          19.594          -1.594        -0.48574
v  ǁVelocityǁ         0.00084932           25.86           7.593          6.5352
v  Pressure                -524.24          206.08          29.199           33.96
v  k                   1.0102e-010          8.8815        0.083754         0.11207
v  omega                     57.48     2.7336e+008     1.2909e+006           76592
v  TempK                    298.15          363.17          325.31          326.04
v  TurbVisc            2.5312e-018      0.00027101     1.9192e-005     4.9668e-005
v  CourantNb           7.8236e-005          1.2604         0.79126         0.97586
v  FourierNb             0.0032444               1         0.38554        0.089066
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0050935     7.5059e-005      0.00019938

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.05          305.76
v  Yplus               0          2.9454          0.6154         0.46494


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4933               2          1.1768          1.0649


 INSTANT    0.284000000E-02   TIME STEP NUMBER             284
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924424E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14001E-01 0.46903E+01
   Friction velocity        uk    :  0.14001E-01 0.46863E+01
   Dimensionless distance   yplus :  0.94927E-02 0.29455E+01
   Friction thermal sca.    tstar :  0.35190E-03 0.18051E+03
   Rough dim-less th. sca.  tplus :  0.67247E-02 0.20866E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25515E+00      10   0.51698E-05   0.74911E+01 0.42409E+02 
c  Velocity[X]                                      0.20702E+01 
c  Velocity[Y]                                      0.16391E+01 
c  Velocity[Z]                                      0.37818E+01 
c  Pressure     0.15659E-04      18   0.31176E-03   0.16041E-01 0.18166E+02 
c  k            0.41641E-02      12   0.20751E-04   0.41114E-01 0.14519E+03 
c  omega        0.27923E+07       1   0.15164E-06   0.17973E+08 0.64445E+00 
c  TempK        0.91374E+04       7   0.42346E-05   0.19153E+03 0.46762E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.9197e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.306          18.701       0.0091969      -0.0082581
v  Velocity[Y]             -15.392          14.653        0.063859        0.090181
v  Velocity[Z]              -25.68          20.514         -1.5943        -0.48593
v  ǁVelocityǁ         0.00084938          25.862          7.5959          6.5389
v  Pressure                -524.71          206.17          29.278          34.018
v  k                   1.0102e-010          8.8809        0.084158         0.11288
v  omega                     57.48     2.7336e+008     1.2909e+006           76595
v  TempK                    298.15          363.17          325.36          326.14
v  TurbVisc            2.5314e-018       0.0002699     1.9277e-005     4.9981e-005
v  CourantNb           7.8469e-005          1.2627          0.7914         0.97588
v  FourierNb             0.0032657               1         0.38555        0.089201
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0050052     7.5029e-005       0.0001993

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.05          305.77
v  Yplus               0          2.9455         0.61567         0.46525


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70087               2          1.1769          1.0651


 INSTANT    0.285000000E-02   TIME STEP NUMBER             285
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924231E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13904E-01 0.46905E+01
   Friction velocity        uk    :  0.13904E-01 0.46865E+01
   Dimensionless distance   yplus :  0.94270E-02 0.29457E+01
   Friction thermal sca.    tstar :  0.38711E-03 0.18177E+03
   Rough dim-less th. sca.  tplus :  0.66781E-02 0.20867E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25543E+00      10   0.51739E-05   0.74306E+01 0.42173E+02 
c  Velocity[X]                                      0.20644E+01 
c  Velocity[Y]                                      0.16345E+01 
c  Velocity[Z]                                      0.37317E+01 
c  Pressure     0.15034E-04      19   0.30659E-03   0.15392E-01 0.18845E+02 
c  k            0.41927E-02      12   0.20444E-04   0.40874E-01 0.14397E+03 
c  omega        0.27923E+07       1   0.15006E-06   0.16125E+08 0.61723E+00 
c  TempK        0.91459E+04       7   0.42293E-05   0.19051E+03 0.46494E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.9059e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.304          18.707       0.0091883      -0.0082196
v  Velocity[Y]             -15.289           14.66        0.064059        0.090556
v  Velocity[Z]             -25.683          20.058         -1.5946        -0.48611
v  ǁVelocityǁ         0.00084952          25.865          7.5987          6.5426
v  Pressure                -525.22          206.26          29.362          34.082
v  k                   1.0103e-010          8.8801        0.084562          0.1137
v  omega                    57.481     2.7336e+008      1.291e+006           76597
v  TempK                    298.15          363.17          325.41          326.23
v  TurbVisc            2.5315e-018      0.00026881     1.9362e-005     5.0299e-005
v  CourantNb           7.8779e-005          1.2649         0.79154          0.9759
v  FourierNb             0.0032871               1         0.38556        0.089341
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0049205     7.4999e-005      0.00019922

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.06          305.77
v  Yplus               0          2.9457         0.61594         0.46556


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40119               2          1.1771          1.0652


 INSTANT    0.286000000E-02   TIME STEP NUMBER             286
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924350E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13820E-01 0.46906E+01
   Friction velocity        uk    :  0.13820E-01 0.46866E+01
   Dimensionless distance   yplus :  0.93702E-02 0.29458E+01
   Friction thermal sca.    tstar :  0.42574E-03 0.18287E+03
   Rough dim-less th. sca.  tplus :  0.66379E-02 0.20868E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25570E+00      10   0.51679E-05   0.73730E+01 0.41952E+02 
c  Velocity[X]                                      0.20599E+01 
c  Velocity[Y]                                      0.16325E+01 
c  Velocity[Z]                                      0.36807E+01 
c  Pressure     0.16440E-04      19   0.31142E-03   0.16821E-01 0.17769E+02 
c  k            0.42213E-02      12   0.20180E-04   0.40636E-01 0.14275E+03 
c  omega        0.27923E+07       1   0.14830E-06   0.12657E+08 0.55962E+00 
c  TempK        0.91544E+04       7   0.42240E-05   0.18952E+03 0.46232E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8917e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.302          18.713        0.009177      -0.0081797
v  Velocity[Y]             -15.255          14.672        0.064262        0.090931
v  Velocity[Z]             -25.686          20.167          -1.595        -0.48631
v  ǁVelocityǁ         0.00084964          25.868          7.6015          6.5463
v  Pressure                -525.75          206.35          29.437          34.137
v  k                   1.0103e-010          8.8791        0.084965         0.11452
v  omega                    57.481     2.7336e+008      1.291e+006           76600
v  TempK                    298.15          363.17          325.47          326.32
v  TurbVisc            2.5316e-018      0.00026773     1.9447e-005     5.0622e-005
v  CourantNb            7.913e-005          1.2672         0.79168         0.97592
v  FourierNb             0.0033085               1         0.38557        0.089485
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0048134      7.497e-005      0.00019915

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.06          305.77
v  Yplus               0          2.9458         0.61621         0.46587


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73123               2          1.1773          1.0654


 INSTANT    0.287000000E-02   TIME STEP NUMBER             287
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924212E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13744E-01 0.46907E+01
   Friction velocity        uk    :  0.13744E-01 0.46868E+01
   Dimensionless distance   yplus :  0.93186E-02 0.29460E+01
   Friction thermal sca.    tstar :  0.46810E-03 0.18388E+03
   Rough dim-less th. sca.  tplus :  0.66014E-02 0.20870E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25597E+00      10   0.51291E-05   0.72997E+01 0.41726E+02 
c  Velocity[X]                                      0.20519E+01 
c  Velocity[Y]                                      0.16297E+01 
c  Velocity[Z]                                      0.36181E+01 
c  Pressure     0.14990E-04      19   0.30625E-03   0.15328E-01 0.18282E+02 
c  k            0.42501E-02      12   0.19733E-04   0.40407E-01 0.14153E+03 
c  omega        0.27923E+07       1   0.14716E-06   0.12235E+08 0.55591E+00 
c  TempK        0.91628E+04       7   0.42186E-05   0.18854E+03 0.45974E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8773e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -18.3          18.719       0.0091634      -0.0081452
v  Velocity[Y]             -15.278          14.685        0.064471        0.091308
v  Velocity[Z]             -25.689          19.791         -1.5953        -0.48651
v  ǁVelocityǁ         0.00084986          25.871          7.6043          6.5499
v  Pressure                 -526.3          206.44          29.518          34.197
v  k                   1.0104e-010          8.8781        0.085367         0.11535
v  omega                    57.482     2.7336e+008      1.291e+006           76603
v  TempK                    298.15          363.17          325.52          326.42
v  TurbVisc            2.5317e-018      0.00026666     1.9532e-005      5.095e-005
v  CourantNb           7.9429e-005          1.2695         0.79181         0.97594
v  FourierNb             0.0033299               1         0.38559        0.089634
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046897     7.4942e-005      0.00019907

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.07          305.77
v  Yplus               0           2.946         0.61648         0.46618


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68056               2          1.1774          1.0656


 INSTANT    0.288000000E-02   TIME STEP NUMBER             288
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924198E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13677E-01 0.46909E+01
   Friction velocity        uk    :  0.13677E-01 0.46869E+01
   Dimensionless distance   yplus :  0.92731E-02 0.29462E+01
   Friction thermal sca.    tstar :  0.51450E-03 0.18479E+03
   Rough dim-less th. sca.  tplus :  0.65692E-02 0.20871E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25625E+00      10   0.51621E-05   0.72380E+01 0.41508E+02 
c  Velocity[X]                                      0.20445E+01 
c  Velocity[Y]                                      0.16282E+01 
c  Velocity[Z]                                      0.35653E+01 
c  Pressure     0.15958E-04      19   0.30839E-03   0.16307E-01 0.18271E+02 
c  k            0.42790E-02      12   0.19483E-04   0.40178E-01 0.14032E+03 
c  omega        0.27923E+07       1   0.14694E-06   0.15369E+08 0.61450E+00 
c  TempK        0.91711E+04       7   0.42134E-05   0.18759E+03 0.45722E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8626e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.298          18.726       0.0091454      -0.0081082
v  Velocity[Y]             -15.355          14.699        0.064681         0.09168
v  Velocity[Z]             -25.692          20.267         -1.5957        -0.48672
v  ǁVelocityǁ            0.00085          25.874          7.6071          6.5535
v  Pressure                -526.86          206.53            29.6          34.258
v  k                   1.0104e-010          8.8769        0.085767         0.11619
v  omega                    57.482     2.7336e+008      1.291e+006           76606
v  TempK                    298.15          363.17          325.57          326.51
v  TurbVisc            2.5318e-018      0.00026803     1.9619e-005     5.1282e-005
v  CourantNb           7.9753e-005          1.2718         0.79195         0.97595
v  FourierNb             0.0033512               1          0.3856        0.089787
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044635     7.4916e-005        0.000199

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.08          305.78
v  Yplus               0          2.9462         0.61674         0.46649


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48638               2          1.1775          1.0657


 INSTANT    0.289000000E-02   TIME STEP NUMBER             289
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924440E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13625E-01 0.46910E+01
   Friction velocity        uk    :  0.13625E-01 0.46871E+01
   Dimensionless distance   yplus :  0.92379E-02 0.29464E+01
   Friction thermal sca.    tstar :  0.56541E-03 0.18549E+03
   Rough dim-less th. sca.  tplus :  0.65442E-02 0.20872E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25652E+00      10   0.51444E-05   0.71743E+01 0.41307E+02 
c  Velocity[X]                                      0.20345E+01 
c  Velocity[Y]                                      0.16285E+01 
c  Velocity[Z]                                      0.35113E+01 
c  Pressure     0.14772E-04      20   0.30001E-03   0.15086E-01 0.17680E+02 
c  k            0.43081E-02      12   0.19251E-04   0.39952E-01 0.13910E+03 
c  omega        0.27923E+07       1   0.14643E-06   0.17059E+08 0.63995E+00 
c  TempK        0.91794E+04       7   0.42075E-05   0.18665E+03 0.45476E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8478e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.296          18.732       0.0091316      -0.0080738
v  Velocity[Y]              -15.42          14.717        0.064893        0.092054
v  Velocity[Z]             -25.695          19.648         -1.5961        -0.48692
v  ǁVelocityǁ         0.00085034          25.877          7.6098           6.557
v  Pressure                -527.44          206.61          29.675          34.313
v  k                   1.0105e-010          8.8755        0.086167         0.11704
v  omega                    57.483     2.7335e+008      1.291e+006           76608
v  TempK                    298.15          363.17          325.62           326.6
v  TurbVisc             2.532e-018      0.00027175     1.9705e-005     5.1617e-005
v  CourantNb           7.9989e-005          1.2742         0.79208         0.97597
v  FourierNb             0.0033726               1         0.38562        0.089943
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044585     7.4889e-005      0.00019893

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.08          305.78
v  Yplus               0          2.9464         0.61701          0.4668


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74293               2          1.1777          1.0659


 INSTANT    0.290000000E-02   TIME STEP NUMBER             290
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924403E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13577E-01 0.46912E+01
   Friction velocity        uk    :  0.13577E-01 0.46872E+01
   Dimensionless distance   yplus :  0.92056E-02 0.29465E+01
   Friction thermal sca.    tstar :  0.62131E-03 0.18614E+03
   Rough dim-less th. sca.  tplus :  0.65213E-02 0.20874E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25679E+00      10   0.51477E-05   0.71172E+01 0.41123E+02 
c  Velocity[X]                                      0.20275E+01 
c  Velocity[Y]                                      0.16318E+01 
c  Velocity[Z]                                      0.34578E+01 
c  Pressure     0.15664E-04      20   0.30256E-03   0.15985E-01 0.19467E+02 
c  k            0.43373E-02      12   0.19000E-04   0.39718E-01 0.13786E+03 
c  omega        0.27923E+07       1   0.14584E-06   0.19255E+08 0.67603E+00 
c  TempK        0.91877E+04       7   0.42016E-05   0.18573E+03 0.45237E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8341e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.294          18.738       0.0091113       -0.008039
v  Velocity[Y]             -15.388          14.789        0.065112        0.092428
v  Velocity[Z]             -25.698          20.379         -1.5966        -0.48714
v  ǁVelocityǁ         0.00085083           25.88          7.6125          6.5606
v  Pressure                -528.03          206.72          29.768          34.384
v  k                   1.0105e-010          8.8736        0.086565         0.11789
v  omega                    57.483     2.7335e+008      1.291e+006           76611
v  TempK                    298.15          363.17          325.67          326.69
v  TurbVisc            2.5321e-018      0.00027539     1.9791e-005     5.1957e-005
v  CourantNb           8.0308e-005          1.2765         0.79221         0.97599
v  FourierNb             0.0033941               1         0.38563        0.090103
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044514     7.4865e-005      0.00019886

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.09          305.78
v  Yplus               0          2.9465         0.61727         0.46711


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38486               2          1.1778          1.0661


 INSTANT    0.291000000E-02   TIME STEP NUMBER             291
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924491E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13535E-01 0.46914E+01
   Friction velocity        uk    :  0.13535E-01 0.46874E+01
   Dimensionless distance   yplus :  0.91769E-02 0.29467E+01
   Friction thermal sca.    tstar :  0.68264E-03 0.18672E+03
   Rough dim-less th. sca.  tplus :  0.65010E-02 0.20875E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25706E+00      10   0.51247E-05   0.70508E+01 0.40903E+02 
c  Velocity[X]                                      0.20177E+01 
c  Velocity[Y]                                      0.16309E+01 
c  Velocity[Z]                                      0.34022E+01 
c  Pressure     0.15601E-04      19   0.29682E-03   0.15910E-01 0.18307E+02 
c  k            0.43666E-02      12   0.18768E-04   0.39477E-01 0.13660E+03 
c  omega        0.27923E+07       1   0.14639E-06   0.27849E+08 0.80189E+00 
c  TempK        0.91960E+04       7   0.41955E-05   0.18483E+03 0.45004E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8206e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.292          18.744       0.0090961       -0.008008
v  Velocity[Y]             -15.293          14.791        0.065336        0.092804
v  Velocity[Z]             -25.701          19.496          -1.597        -0.48736
v  ǁVelocityǁ         0.00085129          25.883          7.6151           6.564
v  Pressure                -528.65          206.81          29.849          34.445
v  k                   1.0106e-010          8.8714        0.086962         0.11875
v  omega                    57.484     2.7335e+008      1.291e+006           76614
v  TempK                    298.15          363.17          325.72          326.79
v  TurbVisc            2.5323e-018      0.00027888     1.9878e-005     5.2303e-005
v  CourantNb            8.066e-005          1.2787         0.79234         0.97601
v  FourierNb             0.0034158               1         0.38565        0.090268
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044419     7.4839e-005       0.0001988

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.09          305.79
v  Yplus               0          2.9467         0.61753         0.46742


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65627               2           1.178          1.0663


 INSTANT    0.292000000E-02   TIME STEP NUMBER             292
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924415E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13506E-01 0.46915E+01
   Friction velocity        uk    :  0.13506E-01 0.46875E+01
   Dimensionless distance   yplus :  0.91571E-02 0.29468E+01
   Friction thermal sca.    tstar :  0.74984E-03 0.18713E+03
   Rough dim-less th. sca.  tplus :  0.64869E-02 0.20876E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25733E+00      10   0.50980E-05   0.69726E+01 0.40644E+02 
c  Velocity[X]                                      0.20083E+01 
c  Velocity[Y]                                      0.16266E+01 
c  Velocity[Z]                                      0.33378E+01 
c  Pressure     0.15607E-04      19   0.30039E-03   0.15905E-01 0.17777E+02 
c  k            0.43961E-02      12   0.18602E-04   0.39236E-01 0.13538E+03 
c  omega        0.27923E+07       1   0.14270E-06   0.15143E+08 0.59952E+00 
c  TempK        0.92042E+04       7   0.41899E-05   0.18394E+03 0.44777E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.8067e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.291           18.75       0.0090759      -0.0079765
v  Velocity[Y]             -15.266          14.712        0.065564        0.093179
v  Velocity[Z]             -25.704          20.413         -1.5975        -0.48758
v  ǁVelocityǁ         0.00085184          25.885          7.6178          6.5674
v  Pressure                -529.27          206.89          29.927          34.504
v  k                   1.0107e-010          8.8686        0.087358         0.11962
v  omega                    57.484     2.7335e+008      1.291e+006           76616
v  TempK                    298.15          363.17          325.76          326.88
v  TurbVisc            2.5324e-018      0.00028225     1.9966e-005     5.2653e-005
v  CourantNb           8.0981e-005           1.281         0.79247         0.97602
v  FourierNb             0.0034377               1         0.38567        0.090436
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044304     7.4815e-005      0.00019873

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           304.1          305.79
v  Yplus               0          2.9468         0.61779         0.46773


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49902               2          1.1781          1.0665


 INSTANT    0.293000000E-02   TIME STEP NUMBER             293
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924344E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13488E-01 0.46917E+01
   Friction velocity        uk    :  0.13488E-01 0.46877E+01
   Dimensionless distance   yplus :  0.91452E-02 0.29470E+01
   Friction thermal sca.    tstar :  0.82343E-03 0.18737E+03
   Rough dim-less th. sca.  tplus :  0.64785E-02 0.20877E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25760E+00      10   0.50294E-05   0.68993E+01 0.40400E+02 
c  Velocity[X]                                      0.19961E+01 
c  Velocity[Y]                                      0.16226E+01 
c  Velocity[Z]                                      0.32806E+01 
c  Pressure     0.14700E-04      19   0.29838E-03   0.14970E-01 0.17797E+02 
c  k            0.44258E-02      12   0.18306E-04   0.38990E-01 0.13417E+03 
c  omega        0.27923E+07       1   0.14094E-06   0.12052E+08 0.53667E+00 
c  TempK        0.92123E+04       7   0.41841E-05   0.18305E+03 0.44555E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.7929e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.289          18.756       0.0090546      -0.0079506
v  Velocity[Y]             -15.292          14.693        0.065794        0.093551
v  Velocity[Z]             -25.707          20.025         -1.5979        -0.48781
v  ǁVelocityǁ         0.00085222          25.888          7.6204          6.5708
v  Pressure                -529.91          206.98          30.006          34.563
v  k                   1.0107e-010          8.8652        0.087753         0.12049
v  omega                    57.485     2.7335e+008      1.291e+006           76619
v  TempK                    298.15          363.17          325.81          326.97
v  TurbVisc            2.5326e-018      0.00028548     2.0054e-005     5.3008e-005
v  CourantNb           8.1296e-005          1.2832          0.7926         0.97604
v  FourierNb             0.0034598               1         0.38568        0.090607
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044172     7.4789e-005      0.00019867

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           304.1          305.79
v  Yplus               0           2.947         0.61804         0.46804


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65283               2          1.1783          1.0666


 INSTANT    0.294000000E-02   TIME STEP NUMBER             294
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924427E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13481E-01 0.46919E+01
   Friction velocity        uk    :  0.13481E-01 0.46879E+01
   Dimensionless distance   yplus :  0.91401E-02 0.29472E+01
   Friction thermal sca.    tstar :  0.90402E-03 0.18747E+03
   Rough dim-less th. sca.  tplus :  0.64749E-02 0.20878E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25786E+00      10   0.49606E-05   0.68304E+01 0.40185E+02 
c  Velocity[X]                                      0.19841E+01 
c  Velocity[Y]                                      0.16201E+01 
c  Velocity[Z]                                      0.32261E+01 
c  Pressure     0.14614E-04      19   0.29639E-03   0.14872E-01 0.17448E+02 
c  k            0.44555E-02      12   0.18055E-04   0.38757E-01 0.13297E+03 
c  omega        0.27923E+07       1   0.14093E-06   0.15337E+08 0.59605E+00 
c  TempK        0.92204E+04       7   0.41782E-05   0.18218E+03 0.44340E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.7787e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.287          18.761       0.0090297       -0.007923
v  Velocity[Y]             -15.389          14.711        0.066023        0.093921
v  Velocity[Z]              -25.71          19.925         -1.5984        -0.48804
v  ǁVelocityǁ         0.00085289          25.891           7.623          6.5742
v  Pressure                -530.52          207.07          30.084           34.62
v  k                   1.0108e-010          8.8612        0.088146         0.12138
v  omega                    57.485     2.7335e+008      1.291e+006           76622
v  TempK                    298.15          363.17          325.86          327.06
v  TurbVisc            2.5327e-018       0.0002886     2.0142e-005     5.3369e-005
v  CourantNb           8.1549e-005          1.2856         0.79273         0.97605
v  FourierNb             0.0034823               1          0.3857        0.090782
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.004349     7.4765e-005       0.0001986

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.11          305.79
v  Yplus               0          2.9472          0.6183         0.46835


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43695               2          1.1784          1.0668


 INSTANT    0.295000000E-02   TIME STEP NUMBER             295
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924445E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13486E-01 0.46921E+01
   Friction velocity        uk    :  0.13486E-01 0.46881E+01
   Dimensionless distance   yplus :  0.91436E-02 0.29474E+01
   Friction thermal sca.    tstar :  0.99223E-03 0.18740E+03
   Rough dim-less th. sca.  tplus :  0.64774E-02 0.20879E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25813E+00      10   0.49300E-05   0.67633E+01 0.39983E+02 
c  Velocity[X]                                      0.19728E+01 
c  Velocity[Y]                                      0.16186E+01 
c  Velocity[Z]                                      0.31719E+01 
c  Pressure     0.14436E-04      20   0.29541E-03   0.14681E-01 0.17521E+02 
c  k            0.44854E-02      12   0.17833E-04   0.38523E-01 0.13175E+03 
c  omega        0.27923E+07       1   0.14040E-06   0.17064E+08 0.62431E+00 
c  TempK        0.92285E+04       7   0.41723E-05   0.18130E+03 0.44131E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.7644e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.286          18.767       0.0090057      -0.0078979
v  Velocity[Y]             -15.449          14.736        0.066249        0.094288
v  Velocity[Z]             -25.713          19.716          -1.599        -0.48828
v  ǁVelocityǁ          0.0008534          25.894          7.6255          6.5775
v  Pressure                -531.09          207.15          30.161          34.678
v  k                   1.0108e-010          8.8566        0.088538         0.12227
v  omega                    57.486     2.7335e+008      1.291e+006           76625
v  TempK                    298.15          363.17          325.91          327.15
v  TurbVisc            2.5329e-018      0.00029161     2.0231e-005     5.3735e-005
v  CourantNb           8.1857e-005          1.2879         0.79285         0.97607
v  FourierNb             0.0035051               1         0.38572        0.090962
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0042423     7.4741e-005      0.00019854

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.11           305.8
v  Yplus               0          2.9474         0.61856         0.46867


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58973               2          1.1786           1.067


 INSTANT    0.296000000E-02   TIME STEP NUMBER             296
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924425E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13501E-01 0.46923E+01
   Friction velocity        uk    :  0.13501E-01 0.46883E+01
   Dimensionless distance   yplus :  0.91542E-02 0.29475E+01
   Friction thermal sca.    tstar :  0.10887E-02 0.18718E+03
   Rough dim-less th. sca.  tplus :  0.64849E-02 0.20881E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25839E+00      10   0.49133E-05   0.66920E+01 0.39766E+02 
c  Velocity[X]                                      0.19600E+01 
c  Velocity[Y]                                      0.16177E+01 
c  Velocity[Z]                                      0.31143E+01 
c  Pressure     0.14571E-04      19   0.29060E-03   0.14808E-01 0.17150E+02 
c  k            0.45155E-02      12   0.17681E-04   0.38307E-01 0.13053E+03 
c  omega        0.27923E+07       1   0.13931E-06   0.15438E+08 0.59727E+00 
c  TempK        0.92365E+04       7   0.41664E-05   0.18043E+03 0.43925E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.7512e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.284          18.772       0.0089772      -0.0078729
v  Velocity[Y]             -15.379          14.759        0.066478        0.094654
v  Velocity[Z]             -25.716          19.926         -1.5995        -0.48852
v  ǁVelocityǁ         0.00085421          25.898          7.6281          6.5807
v  Pressure                -531.67          207.24          30.236          34.733
v  k                   1.0109e-010          8.8513        0.088929         0.12316
v  omega                    57.486     2.7334e+008      1.291e+006           76627
v  TempK                    298.15          363.17          325.96          327.24
v  TurbVisc             2.533e-018      0.00029455      2.032e-005     5.4105e-005
v  CourantNb           8.2118e-005          1.2901         0.79298         0.97609
v  FourierNb             0.0035282               1         0.38574        0.091144
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0041485     7.4717e-005      0.00019848

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.12           305.8
v  Yplus               0          2.9475         0.61882         0.46898


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41298               2          1.1787          1.0672


 INSTANT    0.297000000E-02   TIME STEP NUMBER             297
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924213E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13532E-01 0.46925E+01
   Friction velocity        uk    :  0.13532E-01 0.46885E+01
   Dimensionless distance   yplus :  0.91751E-02 0.29477E+01
   Friction thermal sca.    tstar :  0.11740E-02 0.18676E+03
   Rough dim-less th. sca.  tplus :  0.64997E-02 0.20882E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25865E+00      10   0.49154E-05   0.66157E+01 0.39498E+02 
c  Velocity[X]                                      0.19461E+01 
c  Velocity[Y]                                      0.16107E+01 
c  Velocity[Z]                                      0.30590E+01 
c  Pressure     0.14889E-04      18   0.28910E-03   0.15120E-01 0.17797E+02 
c  k            0.45456E-02      12   0.17442E-04   0.38100E-01 0.12931E+03 
c  omega        0.27923E+07       1   0.13764E-06   0.11398E+08 0.51666E+00 
c  TempK        0.92445E+04       7   0.41602E-05   0.17955E+03 0.43724E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.7379e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.283          18.778       0.0089477      -0.0078499
v  Velocity[Y]             -15.321          14.778        0.066708        0.095019
v  Velocity[Z]              -25.72          19.567            -1.6        -0.48877
v  ǁVelocityǁ         0.00085486          25.901          7.6306           6.584
v  Pressure                -532.23          207.32          30.316          34.794
v  k                    1.011e-010          8.8454        0.089318         0.12406
v  omega                    57.487     2.7334e+008      1.291e+006           76630
v  TempK                    298.15          363.17          326.01          327.33
v  TurbVisc            2.5332e-018      0.00029741      2.041e-005      5.448e-005
v  CourantNb           8.2432e-005          1.2923          0.7931          0.9761
v  FourierNb             0.0035517               1         0.38575        0.091329
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0041242     7.4693e-005      0.00019842

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.12           305.8
v  Yplus               0          2.9477         0.61908          0.4693


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52528               2          1.1789          1.0674


 INSTANT    0.298000000E-02   TIME STEP NUMBER             298
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924321E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13582E-01 0.46927E+01
   Friction velocity        uk    :  0.13582E-01 0.46887E+01
   Dimensionless distance   yplus :  0.92086E-02 0.29479E+01
   Friction thermal sca.    tstar :  0.12594E-02 0.18608E+03
   Rough dim-less th. sca.  tplus :  0.65234E-02 0.20883E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25891E+00      10   0.48911E-05   0.65463E+01 0.39278E+02 
c  Velocity[X]                                      0.19321E+01 
c  Velocity[Y]                                      0.16073E+01 
c  Velocity[Z]                                      0.30069E+01 
c  Pressure     0.15059E-04      19   0.28872E-03   0.15282E-01 0.17786E+02 
c  k            0.45760E-02      12   0.17154E-04   0.37902E-01 0.12812E+03 
c  omega        0.27923E+07       1   0.13760E-06   0.13409E+08 0.55696E+00 
c  TempK        0.92524E+04       7   0.41540E-05   0.17866E+03 0.43527E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.7246e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.282          18.783       0.0089156      -0.0078261
v  Velocity[Y]             -15.311          14.852        0.066945        0.095385
v  Velocity[Z]             -25.723          19.934         -1.6006        -0.48902
v  ǁVelocityǁ         0.00085587          25.905          7.6331          6.5872
v  Pressure                -532.79          207.42          30.396          34.854
v  k                    1.011e-010          8.8389        0.089706         0.12497
v  omega                    57.487     2.7334e+008      1.291e+006           76633
v  TempK                    298.15          363.17          326.06          327.42
v  TurbVisc            2.5334e-018      0.00030023       2.05e-005      5.486e-005
v  CourantNb           8.2699e-005          1.2946         0.79322         0.97612
v  FourierNb             0.0035757               1         0.38577        0.091517
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0042344     7.4667e-005      0.00019836

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.13          305.81
v  Yplus               0          2.9479         0.61933         0.46961


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43127               2           1.179          1.0676


 INSTANT    0.299000000E-02   TIME STEP NUMBER             299
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924391E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13639E-01 0.46930E+01
   Friction velocity        uk    :  0.13639E-01 0.46890E+01
   Dimensionless distance   yplus :  0.92474E-02 0.29481E+01
   Friction thermal sca.    tstar :  0.13493E-02 0.18530E+03
   Rough dim-less th. sca.  tplus :  0.65509E-02 0.20885E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25917E+00      10   0.48556E-05   0.64660E+01 0.39052E+02 
c  Velocity[X]                                      0.19180E+01 
c  Velocity[Y]                                      0.16071E+01 
c  Velocity[Z]                                      0.29409E+01 
c  Pressure     0.15156E-04      19   0.28685E-03   0.15369E-01 0.17965E+02 
c  k            0.46064E-02      12   0.17046E-04   0.37723E-01 0.12698E+03 
c  omega        0.27923E+07       1   0.13945E-06   0.24845E+08 0.75103E+00 
c  TempK        0.92603E+04       7   0.41476E-05   0.17779E+03 0.43336E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.7112e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.28          18.788       0.0088848      -0.0078025
v  Velocity[Y]             -15.331          14.839        0.067186        0.095753
v  Velocity[Z]             -25.727           19.38         -1.6012        -0.48927
v  ǁVelocityǁ         0.00085649          25.908          7.6356          6.5903
v  Pressure                -533.36          207.51          30.479          34.917
v  k                   1.0111e-010          8.8317        0.090092         0.12589
v  omega                    57.488     2.7334e+008      1.291e+006           76636
v  TempK                    298.15          363.17          326.11          327.51
v  TurbVisc            2.5335e-018      0.00030301      2.059e-005     5.5243e-005
v  CourantNb           8.3049e-005          1.2968         0.79334         0.97613
v  FourierNb             0.0036002               1         0.38579        0.091708
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044545     7.4644e-005       0.0001983

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.14          305.81
v  Yplus               0          2.9481         0.61959         0.46993


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46959               2          1.1791          1.0678


 INSTANT    0.300000000E-02   TIME STEP NUMBER             300
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924471E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13709E-01 0.46932E+01
   Friction velocity        uk    :  0.13709E-01 0.46892E+01
   Dimensionless distance   yplus :  0.92949E-02 0.29483E+01
   Friction thermal sca.    tstar :  0.14438E-02 0.18435E+03
   Rough dim-less th. sca.  tplus :  0.65846E-02 0.20886E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25943E+00      10   0.48649E-05   0.63878E+01 0.38794E+02 
c  Velocity[X]                                      0.19023E+01 
c  Velocity[Y]                                      0.16008E+01 
c  Velocity[Z]                                      0.28847E+01 
c  Pressure     0.15512E-04      19   0.29029E-03   0.15719E-01 0.17065E+02 
c  k            0.46370E-02      12   0.16811E-04   0.37570E-01 0.12588E+03 
c  omega        0.27923E+07       1   0.13754E-06   0.17780E+08 0.63688E+00 
c  TempK        0.92681E+04       7   0.41410E-05   0.17690E+03 0.43149E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.6973e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.279          18.794        0.008848      -0.0077784
v  Velocity[Y]             -15.434          14.737        0.067426         0.09612
v  Velocity[Z]              -25.73          19.975         -1.6017        -0.48953
v  ǁVelocityǁ         0.00085751          25.911           7.638          6.5934
v  Pressure                -533.94          207.59          30.554          34.974
v  k                   1.0112e-010          8.8238        0.090478         0.12681
v  omega                    57.488     2.7334e+008      1.291e+006           76638
v  TempK                    298.15          363.17          326.16           327.6
v  TurbVisc            2.5337e-018      0.00030472     2.0681e-005     5.5632e-005
v  CourantNb            8.328e-005          1.2991         0.79346         0.97615
v  FourierNb             0.0036252               1         0.38581        0.091902
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045869      7.462e-005      0.00019824

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.14          305.81
v  Yplus               0          2.9483         0.61984         0.47025


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42019               2          1.1793          1.0681


 INSTANT    0.301000000E-02   TIME STEP NUMBER             301
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924413E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13782E-01 0.46935E+01
   Friction velocity        uk    :  0.13782E-01 0.46895E+01
   Dimensionless distance   yplus :  0.93446E-02 0.29485E+01
   Friction thermal sca.    tstar :  0.15432E-02 0.18337E+03
   Rough dim-less th. sca.  tplus :  0.66198E-02 0.20887E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25968E+00      10   0.48672E-05   0.63099E+01 0.38546E+02 
c  Velocity[X]                                      0.18869E+01 
c  Velocity[Y]                                      0.15966E+01 
c  Velocity[Z]                                      0.28263E+01 
c  Pressure     0.14541E-04      19   0.29042E-03   0.14726E-01 0.17454E+02 
c  k            0.46678E-02      12   0.16580E-04   0.37377E-01 0.12480E+03 
c  omega        0.27923E+07       1   0.13832E-06   0.25286E+08 0.75515E+00 
c  TempK        0.92759E+04       7   0.41340E-05   0.17601E+03 0.42966E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.6837e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.278          18.799       0.0088164       -0.007756
v  Velocity[Y]             -15.478          14.693        0.067667        0.096485
v  Velocity[Z]             -25.734          19.193         -1.6023         -0.4898
v  ǁVelocityǁ          0.0008583          25.915          7.6405          6.5965
v  Pressure                -534.52          207.68          30.633          35.034
v  k                   1.0113e-010          8.8153        0.090861         0.12774
v  omega                    57.489     2.7334e+008      1.291e+006           76641
v  TempK                    298.15          363.17          326.21          327.69
v  TurbVisc            2.5339e-018      0.00030556     2.0773e-005     5.6023e-005
v  CourantNb           8.3589e-005          1.3015         0.79358         0.97616
v  FourierNb             0.0036507               1         0.38583        0.092098
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046747     7.4596e-005      0.00019818

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.15          305.82
v  Yplus               0          2.9485          0.6201         0.47056


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48917               2          1.1794          1.0683


 INSTANT    0.302000000E-02   TIME STEP NUMBER             302
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924451E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13871E-01 0.46938E+01
   Friction velocity        uk    :  0.13871E-01 0.46898E+01
   Dimensionless distance   yplus :  0.94046E-02 0.29487E+01
   Friction thermal sca.    tstar :  0.16476E-02 0.18220E+03
   Rough dim-less th. sca.  tplus :  0.66623E-02 0.20888E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.25994E+00      10   0.48176E-05   0.62377E+01 0.38303E+02 
c  Velocity[X]                                      0.18721E+01 
c  Velocity[Y]                                      0.15922E+01 
c  Velocity[Z]                                      0.27734E+01 
c  Pressure     0.15350E-04      19   0.28866E-03   0.15536E-01 0.17360E+02 
c  k            0.46987E-02      12   0.16456E-04   0.37142E-01 0.12371E+03 
c  omega        0.27923E+07       1   0.13543E-06   0.14851E+08 0.58549E+00 
c  TempK        0.92836E+04       7   0.41267E-05   0.17511E+03 0.42788E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      7.671e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.277          18.804       0.0087771      -0.0077346
v  Velocity[Y]             -15.394           14.69         0.06791        0.096848
v  Velocity[Z]             -25.737          20.031          -1.603        -0.49007
v  ǁVelocityǁ         0.00085937          25.918          7.6429          6.5996
v  Pressure                -535.09          207.77          30.712          35.094
v  k                   1.0113e-010           8.806        0.091244         0.12867
v  omega                    57.489     2.7333e+008      1.291e+006           76644
v  TempK                    298.15          363.17          326.25          327.78
v  TurbVisc            2.5341e-018      0.00030641     2.0864e-005     5.6417e-005
v  CourantNb           8.3839e-005          1.3036          0.7937         0.97618
v  FourierNb             0.0036767               1         0.38585        0.092295
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.004713     7.4571e-005      0.00019813

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.15          305.82
v  Yplus               0          2.9487         0.62035         0.47088


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.29162               2          1.1795          1.0685


 INSTANT    0.303000000E-02   TIME STEP NUMBER             303
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924463E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13983E-01 0.46941E+01
   Friction velocity        uk    :  0.13983E-01 0.46901E+01
   Dimensionless distance   yplus :  0.94805E-02 0.29489E+01
   Friction thermal sca.    tstar :  0.17573E-02 0.18074E+03
   Rough dim-less th. sca.  tplus :  0.67161E-02 0.20890E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26019E+00      10   0.47806E-05   0.61564E+01 0.38022E+02 
c  Velocity[X]                                      0.18534E+01 
c  Velocity[Y]                                      0.15819E+01 
c  Velocity[Z]                                      0.27211E+01 
c  Pressure     0.14337E-04      19   0.28941E-03   0.14501E-01 0.16980E+02 
c  k            0.47297E-02      12   0.16233E-04   0.36889E-01 0.12257E+03 
c  omega        0.27923E+07       1   0.13391E-06   0.11022E+08 0.50654E+00 
c  TempK        0.92913E+04       7   0.41191E-05   0.17420E+03 0.42615E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.6582e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.276          18.809       0.0087414      -0.0077147
v  Velocity[Y]             -15.345          14.703        0.068151        0.097209
v  Velocity[Z]             -25.741          19.419         -1.6036        -0.49035
v  ǁVelocityǁ          0.0008603          25.922          7.6453          6.6026
v  Pressure                -535.68          207.84          30.787           35.15
v  k                   1.0114e-010          8.7961        0.091625         0.12961
v  omega                     57.49     2.7333e+008      1.291e+006           76647
v  TempK                    298.15          363.17           326.3          327.87
v  TurbVisc            2.5343e-018       0.0003073     2.0956e-005     5.6815e-005
v  CourantNb           8.4137e-005          1.3058         0.79382         0.97619
v  FourierNb             0.0037033               1         0.38587        0.092496
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0047269     7.4546e-005      0.00019807

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.16          305.82
v  Yplus               0          2.9489          0.6206          0.4712


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5635               2          1.1797          1.0687


 INSTANT    0.304000000E-02   TIME STEP NUMBER             304
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924482E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14105E-01 0.46943E+01
   Friction velocity        uk    :  0.14104E-01 0.46903E+01
   Dimensionless distance   yplus :  0.95631E-02 0.29491E+01
   Friction thermal sca.    tstar :  0.18728E-02 0.17918E+03
   Rough dim-less th. sca.  tplus :  0.67745E-02 0.20891E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26044E+00      10   0.47656E-05   0.60585E+01 0.37747E+02 
c  Velocity[X]                                      0.18325E+01 
c  Velocity[Y]                                      0.15743E+01 
c  Velocity[Z]                                      0.26517E+01 
c  Pressure     0.14190E-04      19   0.28845E-03   0.14343E-01 0.16936E+02 
c  k            0.47609E-02      12   0.16048E-04   0.36624E-01 0.12140E+03 
c  omega        0.27923E+07       1   0.13366E-06   0.11873E+08 0.52371E+00 
c  TempK        0.92989E+04       7   0.41115E-05   0.17327E+03 0.42444E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.6453e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.274          18.815       0.0087057      -0.0076943
v  Velocity[Y]             -15.345          14.741        0.068398        0.097572
v  Velocity[Z]             -25.745          19.735         -1.6042        -0.49062
v  ǁVelocityǁ         0.00086171          25.926          7.6477          6.6056
v  Pressure                -536.28          207.93          30.863          35.208
v  k                   1.0115e-010          8.7854        0.092005         0.13056
v  omega                     57.49     2.7333e+008      1.291e+006           76649
v  TempK                    298.15          363.17          326.35          327.96
v  TurbVisc            2.5345e-018      0.00030825     2.1048e-005     5.7217e-005
v  CourantNb           8.4399e-005           1.308         0.79393         0.97621
v  FourierNb             0.0037116               1         0.38589        0.092699
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0047281     7.4521e-005      0.00019801

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.16          305.82
v  Yplus               0          2.9491         0.62085         0.47152


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46343               2          1.1798          1.0689


 INSTANT    0.305000000E-02   TIME STEP NUMBER             305
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924253E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14229E-01 0.46946E+01
   Friction velocity        uk    :  0.14228E-01 0.46906E+01
   Dimensionless distance   yplus :  0.96472E-02 0.29493E+01
   Friction thermal sca.    tstar :  0.19942E-02 0.17761E+03
   Rough dim-less th. sca.  tplus :  0.68341E-02 0.20893E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26069E+00      10   0.47301E-05   0.59790E+01 0.37511E+02 
c  Velocity[X]                                      0.18117E+01 
c  Velocity[Y]                                      0.15680E+01 
c  Velocity[Z]                                      0.25993E+01 
c  Pressure     0.14259E-04      19   0.28792E-03   0.14404E-01 0.18985E+02 
c  k            0.47922E-02      12   0.15897E-04   0.36350E-01 0.12020E+03 
c  omega        0.27923E+07       1   0.13515E-06   0.18662E+08 0.64749E+00 
c  TempK        0.93065E+04       7   0.41038E-05   0.17233E+03 0.42277E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.6323e-007                             2


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.273           18.82       0.0086726      -0.0076763
v  Velocity[Y]             -15.388          14.849        0.068651        0.097935
v  Velocity[Z]             -25.749           19.11         -1.6049        -0.49091
v  ǁVelocityǁ         0.00086271           25.93            7.65          6.6085
v  Pressure                -536.86          208.03          30.955          35.282
v  k                   1.0116e-010          8.7741        0.092384         0.13151
v  omega                    57.491     2.7333e+008      1.291e+006           76652
v  TempK                    298.15          363.17           326.4          328.05
v  TurbVisc            2.5347e-018      0.00030926     2.1141e-005     5.7623e-005
v  CourantNb           8.4748e-005          1.3102         0.79405         0.97622
v  FourierNb             0.0037112               1         0.38591        0.092904
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0047231     7.4497e-005      0.00019796

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.17          305.83
v  Yplus               0          2.9493          0.6211         0.47184


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.36123               2            1.18          1.0691


 INSTANT    0.306000000E-02   TIME STEP NUMBER             306
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924461E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14365E-01 0.46949E+01
   Friction velocity        uk    :  0.14365E-01 0.46909E+01
   Dimensionless distance   yplus :  0.97394E-02 0.29495E+01
   Friction thermal sca.    tstar :  0.21222E-02 0.17593E+03
   Rough dim-less th. sca.  tplus :  0.68995E-02 0.20894E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26093E+00      10   0.47139E-05   0.58957E+01 0.37291E+02 
c  Velocity[X]                                      0.17923E+01 
c  Velocity[Y]                                      0.15625E+01 
c  Velocity[Z]                                      0.25408E+01 
c  Pressure     0.14179E-04      19   0.28134E-03   0.14315E-01 0.17364E+02 
c  k            0.48236E-02      12   0.15707E-04   0.36079E-01 0.11901E+03 
c  omega        0.27923E+07       1   0.13582E-06   0.22748E+08 0.71156E+00 
c  TempK        0.93140E+04       7   0.40954E-05   0.17138E+03 0.42113E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      7.619e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.272          18.825       0.0086405      -0.0076568
v  Velocity[Y]             -15.538          14.767          0.0689        0.098296
v  Velocity[Z]             -25.753           19.75         -1.6056         -0.4912
v  ǁVelocityǁ         0.00086404          25.933          7.6524          6.6114
v  Pressure                -537.46          208.12          31.036          35.343
v  k                   1.0117e-010           8.762        0.092762         0.13246
v  omega                    57.491     2.7333e+008      1.291e+006           76655
v  TempK                    298.15          363.17          326.45          328.13
v  TurbVisc            2.5349e-018      0.00031032     2.1234e-005     5.8032e-005
v  CourantNb           8.5003e-005          1.3125         0.79416         0.97623
v  FourierNb             0.0037108               1         0.38593        0.093112
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0047133     7.4473e-005      0.00019791

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.18          305.83
v  Yplus               0          2.9495         0.62135         0.47216


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.3554               2          1.1801          1.0693


 INSTANT    0.307000000E-02   TIME STEP NUMBER             307
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924326E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14484E-01 0.46952E+01
   Friction velocity        uk    :  0.14484E-01 0.46912E+01
   Dimensionless distance   yplus :  0.98207E-02 0.29497E+01
   Friction thermal sca.    tstar :  0.22567E-02 0.17448E+03
   Rough dim-less th. sca.  tplus :  0.69570E-02 0.20896E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26118E+00      10   0.47105E-05   0.58067E+01 0.37006E+02 
c  Velocity[X]                                      0.17713E+01 
c  Velocity[Y]                                      0.15539E+01 
c  Velocity[Z]                                      0.24815E+01 
c  Pressure     0.14258E-04      19   0.28281E-03   0.14388E-01 0.17294E+02 
c  k            0.48552E-02      12   0.15462E-04   0.35807E-01 0.11780E+03 
c  omega        0.27923E+07       1   0.13439E-06   0.20386E+08 0.67625E+00 
c  TempK        0.93214E+04       7   0.40867E-05   0.17042E+03 0.41952E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.6067e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.272          18.831       0.0086102      -0.0076386
v  Velocity[Y]             -15.458          14.694        0.069153        0.098657
v  Velocity[Z]             -25.757          18.895         -1.6063         -0.4915
v  ǁVelocityǁ         0.00086498          25.937          7.6547          6.6143
v  Pressure                -538.07           208.2          31.115          35.404
v  k                   1.0117e-010          8.7492        0.093138         0.13343
v  omega                    57.492     2.7333e+008      1.291e+006           76658
v  TempK                    298.15          363.17           326.5          328.22
v  TurbVisc            2.5351e-018      0.00031142     2.1327e-005     5.8444e-005
v  CourantNb           8.5309e-005          1.3146         0.79427         0.97625
v  FourierNb             0.0037104               1         0.38595        0.093321
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046994     7.4449e-005      0.00019785

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.18          305.83
v  Yplus               0          2.9497         0.62159         0.47248


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40613               2          1.1802          1.0696


 INSTANT    0.308000000E-02   TIME STEP NUMBER             308
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924253E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14644E-01 0.46955E+01
   Friction velocity        uk    :  0.14644E-01 0.46915E+01
   Dimensionless distance   yplus :  0.99286E-02 0.29499E+01
   Friction thermal sca.    tstar :  0.23989E-02 0.17258E+03
   Rough dim-less th. sca.  tplus :  0.70335E-02 0.20897E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26142E+00      10   0.46728E-05   0.57076E+01 0.36675E+02 
c  Velocity[X]                                      0.17467E+01 
c  Velocity[Y]                                      0.15384E+01 
c  Velocity[Z]                                      0.24225E+01 
c  Pressure     0.13466E-04      19   0.27304E-03   0.13580E-01 0.16860E+02 
c  k            0.48869E-02      12   0.15391E-04   0.35547E-01 0.11661E+03 
c  omega        0.27923E+07       1   0.13226E-06   0.14629E+08 0.57258E+00 
c  TempK        0.93288E+04       7   0.40777E-05   0.16943E+03 0.41793E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.5947e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.271          18.837       0.0085797      -0.0076188
v  Velocity[Y]             -15.381          14.649        0.069408        0.099019
v  Velocity[Z]             -25.761          19.598         -1.6069         -0.4918
v  ǁVelocityǁ         0.00086655          25.941           7.657          6.6171
v  Pressure                -538.69          208.28           31.19          35.462
v  k                   1.0118e-010          8.7358        0.093513         0.13439
v  omega                    57.492     2.7333e+008      1.291e+006           76660
v  TempK                    298.15          363.17          326.54          328.31
v  TurbVisc            2.5353e-018      0.00031257      2.142e-005     5.8858e-005
v  CourantNb           8.5531e-005          1.3167         0.79438         0.97626
v  FourierNb             0.0037101               1         0.38597        0.093531
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046834     7.4425e-005       0.0001978

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.19          305.84
v  Yplus               0          2.9499         0.62184         0.47279


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39162               2          1.1804          1.0698


 INSTANT    0.309000000E-02   TIME STEP NUMBER             309
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924127E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14818E-01 0.46958E+01
   Friction velocity        uk    :  0.14818E-01 0.46918E+01
   Dimensionless distance   yplus :  0.10047E-01 0.29501E+01
   Friction thermal sca.    tstar :  0.25500E-02 0.17055E+03
   Rough dim-less th. sca.  tplus :  0.71171E-02 0.20899E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26166E+00      10   0.46117E-05   0.56159E+01 0.36383E+02 
c  Velocity[X]                                      0.17232E+01 
c  Velocity[Y]                                      0.15259E+01 
c  Velocity[Z]                                      0.23668E+01 
c  Pressure     0.13590E-04      19   0.26825E-03   0.13699E-01 0.19078E+02 
c  k            0.49188E-02      12   0.15233E-04   0.35287E-01 0.11540E+03 
c  omega        0.27923E+07       1   0.13059E-06   0.10352E+08 0.48336E+00 
c  TempK        0.93361E+04       7   0.40686E-05   0.16843E+03 0.41635E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.5823e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.27          18.842       0.0085506      -0.0076013
v  Velocity[Y]             -15.355          14.636        0.069666        0.099382
v  Velocity[Z]             -25.765          18.899         -1.6076         -0.4921
v  ǁVelocityǁ         0.00086779          25.946          7.6592          6.6199
v  Pressure                -539.26          208.38          31.285           35.54
v  k                   1.0119e-010          8.7216        0.093887         0.13537
v  omega                    57.493     2.7332e+008      1.291e+006           76663
v  TempK                    298.15          363.17          326.59          328.39
v  TurbVisc            2.5355e-018      0.00031377     2.1514e-005     5.9275e-005
v  CourantNb            8.586e-005          1.3189         0.79449         0.97628
v  FourierNb             0.0037097               1         0.38599        0.093743
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046634     7.4401e-005      0.00019775

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           304.2          305.84
v  Yplus               0          2.9501         0.62208         0.47312


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.29689               2          1.1805            1.07


 INSTANT    0.310000000E-02   TIME STEP NUMBER             310
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924484E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14988E-01 0.46961E+01
   Friction velocity        uk    :  0.14988E-01 0.46921E+01
   Dimensionless distance   yplus :  0.10162E-01 0.29504E+01
   Friction thermal sca.    tstar :  0.27102E-02 0.16861E+03
   Rough dim-less th. sca.  tplus :  0.71990E-02 0.20901E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26190E+00      10   0.45614E-05   0.55249E+01 0.36097E+02 
c  Velocity[X]                                      0.16999E+01 
c  Velocity[Y]                                      0.15137E+01 
c  Velocity[Z]                                      0.23113E+01 
c  Pressure     0.12889E-04      19   0.25637E-03   0.12984E-01 0.16933E+02 
c  k            0.49507E-02      12   0.15126E-04   0.35021E-01 0.11417E+03 
c  omega        0.27923E+07       1   0.13013E-06   0.10145E+08 0.47861E+00 
c  TempK        0.93434E+04       7   0.40590E-05   0.16740E+03 0.41480E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.5696e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.269          18.848       0.0085239      -0.0075844
v  Velocity[Y]             -15.375          14.638        0.069926        0.099746
v  Velocity[Z]              -25.77           19.35         -1.6084        -0.49241
v  ǁVelocityǁ         0.00086938           25.95          7.6615          6.6227
v  Pressure                -539.84          208.47          31.363          35.599
v  k                    1.012e-010          8.7068         0.09426         0.13634
v  omega                    57.493     2.7332e+008     1.2911e+006           76666
v  TempK                    298.15          363.17          326.64          328.48
v  TurbVisc            2.5357e-018      0.00031506     2.1608e-005     5.9697e-005
v  CourantNb           8.6127e-005          1.3211          0.7946         0.97629
v  FourierNb             0.0037093               1         0.38602        0.093957
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006         0.00464     7.4377e-005       0.0001977

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           304.2          305.84
v  Yplus               0          2.9504         0.62233         0.47344


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41935               2          1.1806          1.0702


 INSTANT    0.311000000E-02   TIME STEP NUMBER             311
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924482E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15155E-01 0.46964E+01
   Friction velocity        uk    :  0.15155E-01 0.46924E+01
   Dimensionless distance   yplus :  0.10275E-01 0.29506E+01
   Friction thermal sca.    tstar :  0.28806E-02 0.16676E+03
   Rough dim-less th. sca.  tplus :  0.72790E-02 0.20902E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26214E+00      10   0.45347E-05   0.54245E+01 0.35809E+02 
c  Velocity[X]                                      0.16753E+01 
c  Velocity[Y]                                      0.15017E+01 
c  Velocity[Z]                                      0.22475E+01 
c  Pressure     0.12582E-04      20   0.25615E-03   0.12668E-01 0.18934E+02 
c  k            0.49829E-02      12   0.15132E-04   0.34746E-01 0.11293E+03 
c  omega        0.27923E+07       1   0.13144E-06   0.15563E+08 0.58677E+00 
c  TempK        0.93506E+04       7   0.40493E-05   0.16636E+03 0.41327E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.5567e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.268          18.855       0.0084987      -0.0075704
v  Velocity[Y]             -15.463          14.691        0.070186         0.10011
v  Velocity[Z]             -25.774          18.576         -1.6091        -0.49272
v  ǁVelocityǁ         0.00087061          25.954          7.6637          6.6254
v  Pressure                -540.39          208.56          31.458          35.676
v  k                   1.0121e-010          8.6913        0.094632         0.13733
v  omega                    57.494     2.7332e+008     1.2911e+006           76669
v  TempK                    298.15          363.17          326.69          328.57
v  TurbVisc            2.5359e-018      0.00031641     2.1703e-005     6.0122e-005
v  CourantNb           8.6443e-005          1.3233          0.7947          0.9763
v  FourierNb             0.0037089               1         0.38604        0.094173
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046141     7.4353e-005      0.00019764

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.21          305.85
v  Yplus               0          2.9506         0.62258         0.47376


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47128               2          1.1807          1.0705


 INSTANT    0.312000000E-02   TIME STEP NUMBER             312
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924475E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15324E-01 0.46967E+01
   Friction velocity        uk    :  0.15324E-01 0.46927E+01
   Dimensionless distance   yplus :  0.10390E-01 0.29509E+01
   Friction thermal sca.    tstar :  0.30621E-02 0.16492E+03
   Rough dim-less th. sca.  tplus :  0.73601E-02 0.20904E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26237E+00      10   0.45110E-05   0.53374E+01 0.35567E+02 
c  Velocity[X]                                      0.16516E+01 
c  Velocity[Y]                                      0.14938E+01 
c  Velocity[Z]                                      0.21920E+01 
c  Pressure     0.12245E-04      20   0.24341E-03   0.12322E-01 0.18850E+02 
c  k            0.50152E-02      12   0.14916E-04   0.34469E-01 0.11169E+03 
c  omega        0.27923E+07       1   0.13283E-06   0.22066E+08 0.69529E+00 
c  TempK        0.93578E+04       7   0.40386E-05   0.16530E+03 0.41175E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.5437e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.268          18.862       0.0084764      -0.0075561
v  Velocity[Y]             -15.514          14.727         0.07045         0.10048
v  Velocity[Z]             -25.779          19.032         -1.6099        -0.49303
v  ǁVelocityǁ         0.00087241          25.959           7.666          6.6281
v  Pressure                -540.91          208.67          31.552          35.752
v  k                   1.0122e-010          8.6752        0.095002         0.13831
v  omega                    57.494     2.7332e+008     1.2911e+006           76671
v  TempK                    298.15          363.17          326.74          328.65
v  TurbVisc            2.5361e-018      0.00031784     2.1798e-005      6.055e-005
v  CourantNb           8.6686e-005          1.3256         0.79481         0.97632
v  FourierNb             0.0037086               1         0.38606         0.09439
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045876      7.433e-005      0.00019759

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.21          305.85
v  Yplus               0          2.9509         0.62283         0.47408


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4154               2          1.1809          1.0707


 INSTANT    0.313000000E-02   TIME STEP NUMBER             313
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924288E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15491E-01 0.46970E+01
   Friction velocity        uk    :  0.15491E-01 0.46930E+01
   Dimensionless distance   yplus :  0.10503E-01 0.29511E+01
   Friction thermal sca.    tstar :  0.32569E-02 0.16314E+03
   Rough dim-less th. sca.  tplus :  0.74404E-02 0.20906E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26260E+00      10   0.45366E-05   0.52452E+01 0.35296E+02 
c  Velocity[X]                                      0.16265E+01 
c  Velocity[Y]                                      0.14839E+01 
c  Velocity[Z]                                      0.21347E+01 
c  Pressure     0.12066E-04      20   0.24767E-03   0.12135E-01 0.19086E+02 
c  k            0.50476E-02      12   0.14844E-04   0.34233E-01 0.11055E+03 
c  omega        0.27923E+07       1   0.13179E-06   0.19762E+08 0.65995E+00 
c  TempK        0.93649E+04       7   0.40280E-05   0.16421E+03 0.41023E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.5316e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.267          18.869       0.0084542      -0.0075449
v  Velocity[Y]             -15.438          14.693        0.070715         0.10084
v  Velocity[Z]             -25.783          18.323         -1.6106        -0.49335
v  ǁVelocityǁ         0.00087374          25.963          7.6682          6.6308
v  Pressure                -541.42          208.77          31.649          35.832
v  k                   1.0123e-010          8.6585        0.095371         0.13931
v  omega                    57.495     2.7332e+008     1.2911e+006           76674
v  TempK                    298.15          363.17          326.78          328.74
v  TurbVisc            2.5364e-018      0.00032058     2.1892e-005     6.0978e-005
v  CourantNb            8.702e-005          1.3277         0.79491         0.97633
v  FourierNb             0.0037082               1         0.38609        0.094608
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045617     7.4307e-005      0.00019754

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.22          305.85
v  Yplus               0          2.9511         0.62307          0.4744


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45744               2           1.181          1.0709


 INSTANT    0.314000000E-02   TIME STEP NUMBER             314
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924422E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15691E-01 0.46973E+01
   Friction velocity        uk    :  0.15691E-01 0.46933E+01
   Dimensionless distance   yplus :  0.10639E-01 0.29513E+01
   Friction thermal sca.    tstar :  0.34669E-02 0.16106E+03
   Rough dim-less th. sca.  tplus :  0.75365E-02 0.20907E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26283E+00      10   0.45100E-05   0.51427E+01 0.34933E+02 
c  Velocity[X]                                      0.15997E+01 
c  Velocity[Y]                                      0.14649E+01 
c  Velocity[Z]                                      0.20781E+01 
c  Pressure     0.11910E-04      20   0.25639E-03   0.11972E-01 0.17934E+02 
c  k            0.50802E-02      12   0.14648E-04   0.34012E-01 0.10945E+03 
c  omega        0.27923E+07       1   0.12984E-06   0.13930E+08 0.55378E+00 
c  TempK        0.93719E+04       7   0.40160E-05   0.16310E+03 0.40874E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.5196e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.267          18.876       0.0084319      -0.0075353
v  Velocity[Y]             -15.378          14.659        0.070979         0.10121
v  Velocity[Z]             -25.787          18.666         -1.6114        -0.49367
v  ǁVelocityǁ         0.00087542          25.967          7.6703          6.6334
v  Pressure                -541.92          208.86          31.737          35.903
v  k                   1.0124e-010          8.6412        0.095739          0.1403
v  omega                    57.495     2.7332e+008     1.2911e+006           76677
v  TempK                    298.15          363.17          326.83          328.82
v  TurbVisc            2.5366e-018      0.00032343     2.1987e-005     6.1408e-005
v  CourantNb           8.7265e-005          1.3299         0.79501         0.97634
v  FourierNb             0.0037078               1         0.38611        0.094828
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045428     7.4285e-005      0.00019749

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.23          305.86
v  Yplus               0          2.9513         0.62331         0.47472


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38636               2          1.1811          1.0712


 INSTANT    0.315000000E-02   TIME STEP NUMBER             315
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924431E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15895E-01 0.46976E+01
   Friction velocity        uk    :  0.15895E-01 0.46936E+01
   Dimensionless distance   yplus :  0.10777E-01 0.29516E+01
   Friction thermal sca.    tstar :  0.36957E-02 0.15898E+03
   Rough dim-less th. sca.  tplus :  0.76348E-02 0.20909E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26306E+00      10   0.44989E-05   0.50467E+01 0.34620E+02 
c  Velocity[X]                                      0.15741E+01 
c  Velocity[Y]                                      0.14493E+01 
c  Velocity[Z]                                      0.20233E+01 
c  Pressure     0.11992E-04      19   0.25835E-03   0.12048E-01 0.18695E+02 
c  k            0.51130E-02      12   0.14471E-04   0.33741E-01 0.10826E+03 
c  omega        0.27923E+07       1   0.12863E-06   0.10097E+08 0.47300E+00 
c  TempK        0.93789E+04       7   0.40036E-05   0.16197E+03 0.40725E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.5074e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.266          18.883       0.0084121      -0.0075284
v  Velocity[Y]             -15.364          14.668        0.071245         0.10158
v  Velocity[Z]             -25.792          18.086         -1.6122          -0.494
v  ǁVelocityǁ         0.00087706          25.972          7.6725           6.636
v  Pressure                -542.39          208.96          31.831           35.98
v  k                   1.0124e-010          8.6232        0.096106          0.1413
v  omega                    57.496     2.7332e+008     1.2911e+006           76680
v  TempK                    298.15          363.17          326.88          328.91
v  TurbVisc            2.5368e-018      0.00032629     2.2082e-005     6.1842e-005
v  CourantNb           8.7559e-005           1.332         0.79511         0.97635
v  FourierNb             0.0037075               1         0.38613        0.095048
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045709     7.4263e-005      0.00019745

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.23          305.86
v  Yplus               0          2.9516         0.62355         0.47505


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4068               2          1.1812          1.0714


 INSTANT    0.316000000E-02   TIME STEP NUMBER             316
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924360E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16084E-01 0.46979E+01
   Friction velocity        uk    :  0.16084E-01 0.46939E+01
   Dimensionless distance   yplus :  0.10906E-01 0.29518E+01
   Friction thermal sca.    tstar :  0.39461E-02 0.15711E+03
   Rough dim-less th. sca.  tplus :  0.77255E-02 0.20911E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26328E+00      10   0.44737E-05   0.49564E+01 0.34327E+02 
c  Velocity[X]                                      0.15505E+01 
c  Velocity[Y]                                      0.14347E+01 
c  Velocity[Z]                                      0.19712E+01 
c  Pressure     0.12241E-04      20   0.25505E-03   0.12292E-01 0.18784E+02 
c  k            0.51459E-02      12   0.14380E-04   0.33456E-01 0.10703E+03 
c  omega        0.27923E+07       1   0.12837E-06   0.98489E+07 0.46935E+00 
c  TempK        0.93858E+04       7   0.39903E-05   0.16081E+03 0.40577E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.4949e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.266          18.891       0.0083929      -0.0075231
v  Velocity[Y]             -15.382          14.676        0.071514         0.10196
v  Velocity[Z]             -25.797          18.377         -1.6129        -0.49432
v  ǁVelocityǁ         0.00087877          25.976          7.6746          6.6385
v  Pressure                -542.82          209.06          31.926          36.059
v  k                   1.0125e-010          8.6047        0.096473         0.14231
v  omega                    57.496     2.7332e+008     1.2911e+006           76682
v  TempK                    298.15          363.17          326.93          328.99
v  TurbVisc             2.537e-018      0.00032916     2.2178e-005     6.2277e-005
v  CourantNb           8.7838e-005          1.3342         0.79521         0.97637
v  FourierNb             0.0037072               1         0.38616         0.09527
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045866     7.4241e-005       0.0001974

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.24          305.86
v  Yplus               0          2.9518         0.62379         0.47537


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47111               2          1.1814          1.0716


 INSTANT    0.317000000E-02   TIME STEP NUMBER             317
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924454E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16282E-01 0.46982E+01
   Friction velocity        uk    :  0.16282E-01 0.46942E+01
   Dimensionless distance   yplus :  0.11040E-01 0.29521E+01
   Friction thermal sca.    tstar :  0.42233E-02 0.15520E+03
   Rough dim-less th. sca.  tplus :  0.78206E-02 0.20913E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26351E+00      10   0.44197E-05   0.48695E+01 0.34049E+02 
c  Velocity[X]                                      0.15288E+01 
c  Velocity[Y]                                      0.14198E+01 
c  Velocity[Z]                                      0.19209E+01 
c  Pressure     0.12535E-04      19   0.24184E-03   0.12581E-01 0.19502E+02 
c  k            0.51791E-02      12   0.14295E-04   0.33181E-01 0.10581E+03 
c  omega        0.27923E+07       1   0.12940E-06   0.13064E+08 0.53922E+00 
c  TempK        0.93927E+04       7   0.39767E-05   0.15964E+03 0.40430E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.4821e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.265          18.898        0.008376      -0.0075202
v  Velocity[Y]             -15.483          14.685        0.071781         0.10233
v  Velocity[Z]             -25.802          17.835         -1.6137        -0.49466
v  ǁVelocityǁ         0.00088023          25.981          7.6767           6.641
v  Pressure                -543.23          209.16          32.027          36.142
v  k                   1.0126e-010          8.5856        0.096839         0.14332
v  omega                    57.497     2.7331e+008     1.2911e+006           76685
v  TempK                    298.15          363.17          326.97          329.07
v  TurbVisc            2.5373e-018      0.00033204     2.2273e-005     6.2714e-005
v  CourantNb           8.8122e-005          1.3365         0.79531         0.97638
v  FourierNb             0.0037068               1         0.38619        0.095494
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045941     7.4219e-005      0.00019735

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.25          305.86
v  Yplus               0          2.9521         0.62404          0.4757


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46286               2          1.1815          1.0719


 INSTANT    0.318000000E-02   TIME STEP NUMBER             318
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924337E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16458E-01 0.46985E+01
   Friction velocity        uk    :  0.16458E-01 0.46945E+01
   Dimensionless distance   yplus :  0.11159E-01 0.29523E+01
   Friction thermal sca.    tstar :  0.45337E-02 0.15355E+03
   Rough dim-less th. sca.  tplus :  0.79048E-02 0.20914E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26373E+00      10   0.43647E-05   0.47811E+01 0.33778E+02 
c  Velocity[X]                                      0.15074E+01 
c  Velocity[Y]                                      0.14073E+01 
c  Velocity[Z]                                      0.18664E+01 
c  Pressure     0.12488E-04      19   0.23052E-03   0.12527E-01 0.19930E+02 
c  k            0.52124E-02      12   0.14193E-04   0.32916E-01 0.10463E+03 
c  omega        0.27923E+07       1   0.13197E-06   0.24355E+08 0.73815E+00 
c  TempK        0.93995E+04       7   0.39630E-05   0.15844E+03 0.40284E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.4694e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.265          18.905        0.008361      -0.0075168
v  Velocity[Y]             -15.527          14.693         0.07205          0.1027
v  Velocity[Z]             -25.807          18.024         -1.6146        -0.49499
v  ǁVelocityǁ         0.00088226          25.986          7.6788          6.6435
v  Pressure                -543.59          209.27          32.132           36.23
v  k                   1.0127e-010          8.5661        0.097204         0.14434
v  omega                    57.497     2.7331e+008     1.2911e+006           76688
v  TempK                    298.15          363.17          327.02          329.16
v  TurbVisc            2.5375e-018      0.00033493     2.2369e-005     6.3156e-005
v  CourantNb            8.836e-005          1.3388          0.7954         0.97639
v  FourierNb             0.0037065               1         0.38621        0.095718
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044882     7.4198e-005       0.0001973

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.25          305.87
v  Yplus               0          2.9523         0.62429         0.47603


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51497               2          1.1816          1.0721


 INSTANT    0.319000000E-02   TIME STEP NUMBER             319
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924473E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16650E-01 0.46988E+01
   Friction velocity        uk    :  0.16650E-01 0.46948E+01
   Dimensionless distance   yplus :  0.11289E-01 0.29526E+01
   Friction thermal sca.    tstar :  0.48851E-02 0.15178E+03
   Rough dim-less th. sca.  tplus :  0.79972E-02 0.20916E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26395E+00      10   0.43483E-05   0.46967E+01 0.33512E+02 
c  Velocity[X]                                      0.14857E+01 
c  Velocity[Y]                                      0.13942E+01 
c  Velocity[Z]                                      0.18168E+01 
c  Pressure     0.12402E-04      20   0.22724E-03   0.12436E-01 0.19311E+02 
c  k            0.52459E-02      12   0.14117E-04   0.32648E-01 0.10346E+03 
c  omega        0.27923E+07       1   0.13090E-06   0.18296E+08 0.64106E+00 
c  TempK        0.94063E+04       7   0.39487E-05   0.15721E+03 0.40137E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.4574e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.264          18.911       0.0083461      -0.0075141
v  Velocity[Y]             -15.443          14.701        0.072325         0.10307
v  Velocity[Z]             -25.812          17.587         -1.6154        -0.49532
v  ǁVelocityǁ         0.00088402          25.991          7.6809           6.646
v  Pressure                -543.94          209.37          32.231          36.313
v  k                   1.0128e-010           8.546        0.097568         0.14536
v  omega                    57.498     2.7331e+008     1.2911e+006           76691
v  TempK                    298.15          363.17          327.07          329.24
v  TurbVisc            2.5377e-018      0.00033876     2.2465e-005     6.3601e-005
v  CourantNb           8.8676e-005           1.341         0.79549          0.9764
v  FourierNb             0.0037062               1         0.38624        0.095944
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0043676     7.4176e-005      0.00019726

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.26          305.87
v  Yplus               0          2.9526         0.62453         0.47636


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66038               2          1.1817          1.0723


 INSTANT    0.320000000E-02   TIME STEP NUMBER             320
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924415E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15836E-01 0.46991E+01
   Friction velocity        uk    :  0.15836E-01 0.46951E+01
   Dimensionless distance   yplus :  0.11363E-01 0.29528E+01
   Friction thermal sca.    tstar :  0.52870E-02 0.14990E+03
   Rough dim-less th. sca.  tplus :  0.80495E-02 0.20918E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26416E+00      10   0.43283E-05   0.46073E+01 0.33205E+02 
c  Velocity[X]                                      0.14600E+01 
c  Velocity[Y]                                      0.13777E+01 
c  Velocity[Z]                                      0.17696E+01 
c  Pressure     0.12619E-04      19   0.21823E-03   0.12647E-01 0.20158E+02 
c  k            0.52795E-02      12   0.14029E-04   0.32406E-01 0.10231E+03 
c  omega        0.27923E+07       1   0.13176E-06   0.24354E+08 0.73791E+00 
c  TempK        0.94129E+04       7   0.39337E-05   0.15596E+03 0.39991E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.4453e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.264          18.918       0.0083338      -0.0075103
v  Velocity[Y]             -15.394           14.71        0.072602         0.10345
v  Velocity[Z]             -25.816          17.732         -1.6162        -0.49566
v  ǁVelocityǁ          0.0008863          25.995          7.6829          6.6484
v  Pressure                -544.27          209.49          32.339          36.403
v  k                   1.0129e-010          8.5255        0.097932         0.14638
v  omega                    57.498     2.7331e+008     1.2911e+006           76693
v  TempK                    298.15          363.17          327.12          329.32
v  TurbVisc             2.538e-018      0.00034246     2.2562e-005     6.4049e-005
v  CourantNb           8.8946e-005          1.3431         0.79558         0.97641
v  FourierNb             0.0037058               1         0.38627        0.096172
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0043286     7.4156e-005      0.00019721

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.27          305.87
v  Yplus               0          2.9528         0.62477         0.47669


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.31279               2          1.1819          1.0726


 INSTANT    0.321000000E-02   TIME STEP NUMBER             321
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924425E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17072E-01 0.46994E+01
   Friction velocity        uk    :  0.17072E-01 0.46954E+01
   Dimensionless distance   yplus :  0.11575E-01 0.29531E+01
   Friction thermal sca.    tstar :  0.57515E-02 0.14815E+03
   Rough dim-less th. sca.  tplus :  0.82000E-02 0.20920E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26438E+00      10   0.42958E-05   0.45104E+01 0.32858E+02 
c  Velocity[X]                                      0.14293E+01 
c  Velocity[Y]                                      0.13576E+01 
c  Velocity[Z]                                      0.17234E+01 
c  Pressure     0.11914E-04      19   0.21652E-03   0.11935E-01 0.18684E+02 
c  k            0.53134E-02      12   0.14006E-04   0.32167E-01 0.10118E+03 
c  omega        0.27923E+07       1   0.12931E-06   0.13892E+08 0.56382E+00 
c  TempK        0.94196E+04       7   0.39182E-05   0.15468E+03 0.39845E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      7.433e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.264          18.924       0.0083242      -0.0075079
v  Velocity[Y]             -15.394          14.719        0.072881         0.10383
v  Velocity[Z]             -25.821          17.341          -1.617          -0.496
v  ǁVelocityǁ         0.00088804              26           7.685          6.6508
v  Pressure                -544.59          209.59          32.434          36.482
v  k                    1.013e-010          8.5046        0.098295         0.14741
v  omega                    57.498     2.7331e+008     1.2911e+006           76696
v  TempK                    298.15          363.17          327.16           329.4
v  TurbVisc            2.5382e-018      0.00034604     2.2659e-005     6.4499e-005
v  CourantNb           8.9284e-005          1.3453         0.79567         0.97643
v  FourierNb             0.0037055               1          0.3863          0.0964
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0042899     7.4135e-005      0.00019717

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.27          305.88
v  Yplus               0          2.9531         0.62501         0.47702


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53532               2           1.182          1.0728


 INSTANT    0.322000000E-02   TIME STEP NUMBER             322
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924415E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17165E-01 0.46997E+01
   Friction velocity        uk    :  0.17165E-01 0.46957E+01
   Dimensionless distance   yplus :  0.11638E-01 0.29533E+01
   Friction thermal sca.    tstar :  0.62950E-02 0.14865E+03
   Rough dim-less th. sca.  tplus :  0.82445E-02 0.20922E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26459E+00      10   0.42174E-05   0.43937E+01 0.32487E+02 
c  Velocity[X]                                      0.13963E+01 
c  Velocity[Y]                                      0.13383E+01 
c  Velocity[Z]                                      0.16591E+01 
c  Pressure     0.11458E-04      18   0.21195E-03   0.11473E-01 0.18991E+02 
c  k            0.53474E-02      12   0.13991E-04   0.31921E-01 0.10007E+03 
c  omega        0.27923E+07       1   0.12842E-06   0.10978E+08 0.50543E+00 
c  TempK        0.94261E+04       7   0.39020E-05   0.15338E+03 0.39699E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.4204e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.263           18.93       0.0083157      -0.0075052
v  Velocity[Y]              -15.42          14.728        0.073163         0.10422
v  Velocity[Z]             -25.826          17.394         -1.6178        -0.49634
v  ǁVelocityǁ         0.00089047          26.005           7.687          6.6531
v  Pressure                 -544.9          209.69          32.533          36.565
v  k                   1.0131e-010          8.4833        0.098657         0.14844
v  omega                    57.499     2.7331e+008     1.2911e+006           76699
v  TempK                    298.15          363.17          327.21          329.49
v  TurbVisc            2.5385e-018      0.00034949     2.2756e-005      6.495e-005
v  CourantNb           8.9538e-005          1.3476         0.79576         0.97644
v  FourierNb             0.0037052               1         0.38633        0.096629
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.004251     7.4115e-005      0.00019712

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.28          305.88
v  Yplus               0          2.9533         0.62525         0.47735


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.29976               2          1.1821          1.0731


 INSTANT    0.323000000E-02   TIME STEP NUMBER             323
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924421E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17110E-01 0.47000E+01
   Friction velocity        uk    :  0.17110E-01 0.46959E+01
   Dimensionless distance   yplus :  0.11601E-01 0.29536E+01
   Friction thermal sca.    tstar :  0.68400E-02 0.14912E+03
   Rough dim-less th. sca.  tplus :  0.82182E-02 0.20923E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26480E+00      10   0.41886E-05   0.42989E+01 0.32173E+02 
c  Velocity[X]                                      0.13655E+01 
c  Velocity[Y]                                      0.13200E+01 
c  Velocity[Z]                                      0.16134E+01 
c  Pressure     0.11395E-04      18   0.21000E-03   0.11405E-01 0.19275E+02 
c  k            0.53816E-02      12   0.13825E-04   0.31684E-01 0.98974E+02 
c  omega        0.27923E+07       1   0.12914E-06   0.13193E+08 0.55169E+00 
c  TempK        0.94326E+04       7   0.38853E-05   0.15204E+03 0.39554E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.4075e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.263          18.937       0.0083084      -0.0075024
v  Velocity[Y]             -15.524          14.737         0.07344          0.1046
v  Velocity[Z]             -25.831          17.081         -1.6187        -0.49668
v  ǁVelocityǁ         0.00089218           26.01          7.6889          6.6554
v  Pressure                -545.19           209.8          32.635           36.65
v  k                   1.0132e-010          8.4617        0.099018         0.14948
v  omega                    57.499     2.7331e+008     1.2911e+006           76701
v  TempK                    298.15          363.17          327.26          329.57
v  TurbVisc            2.5387e-018      0.00035281     2.2853e-005     6.5405e-005
v  CourantNb           8.9878e-005            1.35         0.79584         0.97645
v  FourierNb             0.0037049               1         0.38636        0.096859
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0042128     7.4096e-005      0.00019708

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.29          305.88
v  Yplus               0          2.9536         0.62548         0.47768


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35156               2          1.1822          1.0733


 INSTANT    0.324000000E-02   TIME STEP NUMBER             324
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924403E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17071E-01 0.47002E+01
   Friction velocity        uk    :  0.17071E-01 0.46962E+01
   Dimensionless distance   yplus :  0.11575E-01 0.29538E+01
   Friction thermal sca.    tstar :  0.73470E-02 0.14946E+03
   Rough dim-less th. sca.  tplus :  0.81996E-02 0.20925E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26501E+00      10   0.41568E-05   0.41999E+01 0.31859E+02 
c  Velocity[X]                                      0.13346E+01 
c  Velocity[Y]                                      0.13034E+01 
c  Velocity[Z]                                      0.15619E+01 
c  Pressure     0.11140E-04      19   0.20682E-03   0.11146E-01 0.19106E+02 
c  k            0.54160E-02      12   0.13718E-04   0.31455E-01 0.97894E+02 
c  omega        0.27923E+07       1   0.13164E-06   0.24503E+08 0.74538E+00 
c  TempK        0.94391E+04       7   0.38682E-05   0.15068E+03 0.39409E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.3948e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.263          18.943       0.0083049      -0.0075011
v  Velocity[Y]             -15.564          14.746        0.073717         0.10498
v  Velocity[Z]             -25.836          17.075         -1.6195        -0.49703
v  ǁVelocityǁ         0.00089471          26.014          7.6909          6.6577
v  Pressure                -545.47           209.9          32.735          36.734
v  k                   1.0133e-010          8.4398        0.099379         0.15052
v  omega                      57.5     2.7331e+008     1.2911e+006           76704
v  TempK                    298.15          363.17          327.31          329.65
v  TurbVisc            2.5389e-018      0.00035599     2.2951e-005      6.586e-005
v  CourantNb           9.0116e-005          1.3523         0.79593         0.97646
v  FourierNb             0.0037046               1         0.38639         0.09709
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0041768     7.4077e-005      0.00019704

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.29          305.89
v  Yplus               0          2.9538         0.62572         0.47801


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46453               2          1.1823          1.0735


 INSTANT    0.325000000E-02   TIME STEP NUMBER             325
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924441E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17040E-01 0.47005E+01
   Friction velocity        uk    :  0.17040E-01 0.46965E+01
   Dimensionless distance   yplus :  0.11554E-01 0.29541E+01
   Friction thermal sca.    tstar :  0.79493E-02 0.14973E+03
   Rough dim-less th. sca.  tplus :  0.81847E-02 0.20927E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26521E+00      10   0.41249E-05   0.41062E+01 0.31535E+02 
c  Velocity[X]                                      0.13037E+01 
c  Velocity[Y]                                      0.12863E+01 
c  Velocity[Z]                                      0.15162E+01 
c  Pressure     0.11356E-04      19   0.20655E-03   0.11356E-01 0.18967E+02 
c  k            0.54506E-02      12   0.13630E-04   0.31239E-01 0.96839E+02 
c  omega        0.27923E+07       1   0.12980E-06   0.16242E+08 0.61323E+00 
c  TempK        0.94455E+04       7   0.38500E-05   0.14930E+03 0.39264E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.3826e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.263          18.949       0.0082993      -0.0075023
v  Velocity[Y]             -15.477          14.755        0.073998         0.10537
v  Velocity[Z]             -25.841          16.811         -1.6203        -0.49738
v  ǁVelocityǁ         0.00089665          26.019          7.6928          6.6599
v  Pressure                -545.73          210.01          32.836          36.819
v  k                   1.0134e-010          8.4176        0.099739         0.15156
v  omega                      57.5     2.7331e+008     1.2911e+006           76707
v  TempK                    298.15          363.17          327.35          329.73
v  TurbVisc            2.5392e-018      0.00035903     2.3048e-005     6.6316e-005
v  CourantNb           9.0453e-005          1.3545         0.79601         0.97647
v  FourierNb             0.0037043               1         0.38643        0.097321
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0041424     7.4059e-005      0.00019699

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           304.3          305.89
v  Yplus               0          2.9541         0.62596         0.47834


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.36475               2          1.1824          1.0738


 INSTANT    0.326000000E-02   TIME STEP NUMBER             326
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924458E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17021E-01 0.47008E+01
   Friction velocity        uk    :  0.17021E-01 0.46968E+01
   Dimensionless distance   yplus :  0.11541E-01 0.29543E+01
   Friction thermal sca.    tstar :  0.86653E-02 0.14990E+03
   Rough dim-less th. sca.  tplus :  0.81754E-02 0.20929E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26541E+00      10   0.40688E-05   0.40102E+01 0.31190E+02 
c  Velocity[X]                                      0.12737E+01 
c  Velocity[Y]                                      0.12642E+01 
c  Velocity[Z]                                      0.14723E+01 
c  Pressure     0.11279E-04      18   0.20890E-03   0.11275E-01 0.18862E+02 
c  k            0.54853E-02      12   0.13615E-04   0.31036E-01 0.95811E+02 
c  omega        0.27923E+07       1   0.13024E-06   0.17125E+08 0.62634E+00 
c  TempK        0.94518E+04       7   0.38307E-05   0.14789E+03 0.39118E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.3705e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.262          18.955       0.0082958      -0.0075062
v  Velocity[Y]             -15.425          14.807        0.074284         0.10575
v  Velocity[Z]             -25.846          16.724         -1.6212        -0.49772
v  ǁVelocityǁ         0.00089944          26.024          7.6947          6.6621
v  Pressure                   -546          210.11          32.934          36.902
v  k                   1.0135e-010          8.3951          0.1001         0.15261
v  omega                    57.501      2.733e+008     1.2911e+006           76709
v  TempK                    298.15          363.17           327.4          329.81
v  TurbVisc            2.5394e-018      0.00036193     2.3146e-005     6.6774e-005
v  CourantNb           9.0709e-005          1.3568         0.79609         0.97648
v  FourierNb              0.003704               1         0.38646        0.097553
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0041088     7.4041e-005      0.00019695

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.31          305.89
v  Yplus               0          2.9543         0.62619         0.47867


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49063               2          1.1826           1.074


 INSTANT    0.327000000E-02   TIME STEP NUMBER             327
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924470E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17015E-01 0.47010E+01
   Friction velocity        uk    :  0.17015E-01 0.46970E+01
   Dimensionless distance   yplus :  0.11537E-01 0.29545E+01
   Friction thermal sca.    tstar :  0.95312E-02 0.14995E+03
   Rough dim-less th. sca.  tplus :  0.81727E-02 0.20930E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26561E+00       9   0.59788E-05   0.39130E+01 0.30857E+02 
c  Velocity[X]                                      0.12444E+01 
c  Velocity[Y]                                      0.12454E+01 
c  Velocity[Z]                                      0.14231E+01 
c  Pressure     0.11888E-04      18   0.21088E-03   0.11878E-01 0.17589E+02 
c  k            0.55203E-02      12   0.13578E-04   0.30824E-01 0.94779E+02 
c  omega        0.27923E+07       1   0.12942E-06   0.16028E+08 0.60885E+00 
c  TempK        0.94581E+04       7   0.38110E-05   0.14645E+03 0.38972E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.3582e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.262          18.961       0.0082927      -0.0075105
v  Velocity[Y]             -15.423          14.773        0.074571         0.10614
v  Velocity[Z]              -25.85          16.521          -1.622        -0.49807
v  ǁVelocityǁ         0.00083061          26.028          7.6966          6.6643
v  Pressure                -546.26           210.2          33.025          36.976
v  k                   1.0136e-010          8.3725         0.10046         0.15366
v  omega                    57.501      2.733e+008     1.2911e+006           76712
v  TempK                    298.15          363.17          327.45          329.89
v  TurbVisc            2.5397e-018       0.0003647     2.3243e-005     6.7234e-005
v  CourantNb           9.1064e-005           1.359         0.79616         0.97649
v  FourierNb             0.0037037               1          0.3865        0.097786
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0041051     7.4024e-005      0.00019691

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.32           305.9
v  Yplus               0          2.9545         0.62642         0.47899


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.36734               2          1.1827          1.0743


 INSTANT    0.328000000E-02   TIME STEP NUMBER             328
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924459E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17020E-01 0.47013E+01
   Friction velocity        uk    :  0.17020E-01 0.46973E+01
   Dimensionless distance   yplus :  0.11540E-01 0.29548E+01
   Friction thermal sca.    tstar :  0.10588E-01 0.14991E+03
   Rough dim-less th. sca.  tplus :  0.81747E-02 0.20932E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26581E+00       9   0.59076E-05   0.38166E+01 0.30483E+02 
c  Velocity[X]                                      0.12146E+01 
c  Velocity[Y]                                      0.12231E+01 
c  Velocity[Z]                                      0.13788E+01 
c  Pressure     0.11750E-04      18   0.20185E-03   0.11736E-01 0.16938E+02 
c  k            0.55555E-02      12   0.13508E-04   0.30612E-01 0.93750E+02 
c  omega        0.27923E+07       1   0.12849E-06   0.14009E+08 0.57321E+00 
c  TempK        0.94643E+04       7   0.37914E-05   0.14500E+03 0.38826E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.3456e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.262          18.967        0.008292      -0.0075159
v  Velocity[Y]             -15.448          14.782         0.07486         0.10654
v  Velocity[Z]             -25.855          16.395         -1.6228        -0.49843
v  ǁVelocityǁ         0.00090416          26.033          7.6984          6.6665
v  Pressure                 -546.5           210.3          33.111          37.046
v  k                   1.0137e-010          8.3496         0.10081         0.15471
v  omega                    57.501      2.733e+008     1.2911e+006           76714
v  TempK                    298.15          363.17          327.49          329.97
v  TurbVisc            2.5399e-018      0.00036732     2.3341e-005     6.7697e-005
v  CourantNb            9.137e-005          1.3614         0.79624          0.9765
v  FourierNb             0.0037034               1         0.38653        0.098019
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.004108     7.4006e-005      0.00019687

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.32           305.9
v  Yplus               0          2.9548         0.62665         0.47931


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56197               2          1.1828          1.0745


 INSTANT    0.329000000E-02   TIME STEP NUMBER             329
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924391E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17033E-01 0.47015E+01
   Friction velocity        uk    :  0.17033E-01 0.46975E+01
   Dimensionless distance   yplus :  0.11549E-01 0.29550E+01
   Friction thermal sca.    tstar :  0.11882E-01 0.14980E+03
   Rough dim-less th. sca.  tplus :  0.81811E-02 0.20933E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26601E+00       9   0.58729E-05   0.37306E+01 0.30163E+02 
c  Velocity[X]                                      0.11874E+01 
c  Velocity[Y]                                      0.12037E+01 
c  Velocity[Z]                                      0.13395E+01 
c  Pressure     0.12928E-04      18   0.20225E-03   0.12908E-01 0.17472E+02 
c  k            0.55908E-02      12   0.13321E-04   0.30387E-01 0.92729E+02 
c  omega        0.27923E+07       1   0.12786E-06   0.12680E+08 0.54186E+00 
c  TempK        0.94705E+04       7   0.37710E-05   0.14352E+03 0.38680E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.3328e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.262          18.974       0.0082868      -0.0075224
v  Velocity[Y]             -15.551          14.792        0.075147         0.10693
v  Velocity[Z]             -25.859           16.21         -1.6237        -0.49878
v  ǁVelocityǁ         0.00090676          26.037          7.7002          6.6686
v  Pressure                -546.72          210.39          33.201          37.121
v  k                   1.0138e-010          8.3267         0.10117         0.15577
v  omega                    57.502      2.733e+008     1.2911e+006           76717
v  TempK                    298.15          363.17          327.54          330.04
v  TurbVisc            2.5402e-018       0.0003698      2.344e-005      6.816e-005
v  CourantNb           9.1651e-005          1.3637         0.79631         0.97651
v  FourierNb             0.0037031               1         0.38657        0.098253
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0041098     7.3989e-005      0.00019683

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.33           305.9
v  Yplus               0           2.955         0.62687         0.47964


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.31034               2          1.1829          1.0748


 INSTANT    0.330000000E-02   TIME STEP NUMBER             330
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924443E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17063E-01 0.47018E+01
   Friction velocity        uk    :  0.17063E-01 0.46978E+01
   Dimensionless distance   yplus :  0.11569E-01 0.29552E+01
   Friction thermal sca.    tstar :  0.13462E-01 0.14953E+03
   Rough dim-less th. sca.  tplus :  0.81955E-02 0.20935E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26620E+00       9   0.57697E-05   0.36485E+01 0.29869E+02 
c  Velocity[X]                                      0.11628E+01 
c  Velocity[Y]                                      0.11865E+01 
c  Velocity[Z]                                      0.12992E+01 
c  Pressure     0.13160E-04      18   0.19997E-03   0.13136E-01 0.16322E+02 
c  k            0.56263E-02      12   0.13240E-04   0.30171E-01 0.91723E+02 
c  omega        0.27923E+07       1   0.12995E-06   0.23657E+08 0.73169E+00 
c  TempK        0.94766E+04       7   0.37495E-05   0.14202E+03 0.38534E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.3201e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.262          18.981       0.0082856      -0.0075306
v  Velocity[Y]             -15.591          14.801        0.075434         0.10732
v  Velocity[Z]             -25.864          16.034         -1.6245        -0.49913
v  ǁVelocityǁ         0.00090927          26.041           7.702          6.6707
v  Pressure                -546.93          210.47          33.282          37.186
v  k                   1.0139e-010          8.3035         0.10153         0.15683
v  omega                    57.502      2.733e+008     1.2911e+006           76720
v  TempK                    298.15          363.17          327.59          330.12
v  TurbVisc            2.5404e-018      0.00037214     2.3538e-005     6.8626e-005
v  CourantNb           9.1961e-005          1.3661         0.79638         0.97652
v  FourierNb             0.0037029               1         0.38661        0.098486
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0041987     7.3972e-005      0.00019679

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.34          305.91
v  Yplus               0          2.9552          0.6271         0.47995


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67915               2           1.183           1.075


 INSTANT    0.331000000E-02   TIME STEP NUMBER             331
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924243E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17100E-01 0.47020E+01
   Friction velocity        uk    :  0.17100E-01 0.46980E+01
   Dimensionless distance   yplus :  0.11594E-01 0.29555E+01
   Friction thermal sca.    tstar :  0.14828E-01 0.14921E+03
   Rough dim-less th. sca.  tplus :  0.82133E-02 0.20937E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26639E+00       9   0.56781E-05   0.35551E+01 0.29546E+02 
c  Velocity[X]                                      0.11332E+01 
c  Velocity[Y]                                      0.11693E+01 
c  Velocity[Z]                                      0.12526E+01 
c  Pressure     0.12793E-04      18   0.19599E-03   0.12767E-01 0.17365E+02 
c  k            0.56621E-02      12   0.13232E-04   0.29956E-01 0.90725E+02 
c  omega        0.27923E+07       1   0.12717E-06   0.13573E+08 0.56072E+00 
c  TempK        0.94826E+04       7   0.37275E-05   0.14050E+03 0.38387E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      7.308e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.261          18.987       0.0082779        -0.00754
v  Velocity[Y]             -15.503           14.81        0.075724         0.10772
v  Velocity[Z]             -25.868          15.759         -1.6253        -0.49948
v  ǁVelocityǁ         0.00091211          26.046          7.7038          6.6727
v  Pressure                -547.12          210.56          33.372          37.262
v  k                    1.014e-010          8.2803         0.10188         0.15789
v  omega                    57.503      2.733e+008     1.2911e+006           76722
v  TempK                    298.15          363.17          327.64           330.2
v  TurbVisc            2.5407e-018      0.00037433     2.3637e-005     6.9094e-005
v  CourantNb           9.2257e-005          1.3684         0.79645         0.97653
v  FourierNb             0.0037026               1         0.38665         0.09872
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0043178     7.3955e-005      0.00019675

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.34          305.91
v  Yplus               0          2.9555         0.62732         0.48027


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48001               2          1.1831          1.0752


 INSTANT    0.332000000E-02   TIME STEP NUMBER             332
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924469E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17156E-01 0.47022E+01
   Friction velocity        uk    :  0.17156E-01 0.46982E+01
   Dimensionless distance   yplus :  0.11632E-01 0.29557E+01
   Friction thermal sca.    tstar :  0.15762E-01 0.14872E+03
   Rough dim-less th. sca.  tplus :  0.82402E-02 0.20938E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26658E+00       9   0.56061E-05   0.34648E+01 0.29190E+02 
c  Velocity[X]                                      0.11063E+01 
c  Velocity[Y]                                      0.11459E+01 
c  Velocity[Z]                                      0.12125E+01 
c  Pressure     0.11428E-04      19   0.19568E-03   0.11402E-01 0.15836E+02 
c  k            0.56980E-02      12   0.13172E-04   0.29761E-01 0.89767E+02 
c  omega        0.27923E+07       1   0.12625E-06   0.11470E+08 0.51396E+00 
c  TempK        0.94886E+04       7   0.37050E-05   0.13896E+03 0.38240E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      7.296e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.261          18.994         0.00827      -0.0075532
v  Velocity[Y]              -15.45           14.82        0.076017         0.10812
v  Velocity[Z]             -25.873          15.468         -1.6262        -0.49983
v  ǁVelocityǁ         0.00091516           26.05          7.7055          6.6747
v  Pressure                 -547.3          210.65           33.45          37.324
v  k                   1.0141e-010          8.2571         0.10224         0.15895
v  omega                    57.503      2.733e+008     1.2911e+006           76725
v  TempK                    298.15          363.17          327.68          330.28
v  TurbVisc            2.5409e-018      0.00037639     2.3735e-005     6.9563e-005
v  CourantNb           9.2584e-005          1.3706         0.79652         0.97654
v  FourierNb             0.0037024               1         0.38669        0.098954
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0042836     7.3938e-005      0.00019671

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.35          305.91
v  Yplus               0          2.9557         0.62754         0.48058


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71841               2          1.1832          1.0755


 INSTANT    0.333000000E-02   TIME STEP NUMBER             333
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924273E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17227E-01 0.47024E+01
   Friction velocity        uk    :  0.17227E-01 0.46984E+01
   Dimensionless distance   yplus :  0.11680E-01 0.29559E+01
   Friction thermal sca.    tstar :  0.16748E-01 0.14811E+03
   Rough dim-less th. sca.  tplus :  0.82742E-02 0.20940E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26677E+00       9   0.55586E-05   0.33866E+01 0.28908E+02 
c  Velocity[X]                                      0.10808E+01 
c  Velocity[Y]                                      0.11295E+01 
c  Velocity[Z]                                      0.11762E+01 
c  Pressure     0.11867E-04      18   0.18908E-03   0.11837E-01 0.16743E+02 
c  k            0.57340E-02      12   0.13037E-04   0.29569E-01 0.88838E+02 
c  omega        0.27923E+07       1   0.12694E-06   0.14656E+08 0.57730E+00 
c  TempK        0.94945E+04       7   0.36821E-05   0.13740E+03 0.38092E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.2838e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.261          19.001       0.0082613      -0.0075678
v  Velocity[Y]             -15.448          14.829        0.076315         0.10852
v  Velocity[Z]             -25.877          15.082          -1.627        -0.50018
v  ǁVelocityǁ         0.00091814          26.054          7.7072          6.6767
v  Pressure                -547.46          210.74          33.536          37.395
v  k                   1.0142e-010          8.2338         0.10259         0.16002
v  omega                    57.503     2.7329e+008     1.2911e+006           76727
v  TempK                    298.15          363.17          327.73          330.35
v  TurbVisc            2.5412e-018      0.00037887     2.3834e-005     7.0033e-005
v  CourantNb            9.293e-005          1.3729         0.79659         0.97655
v  FourierNb             0.0037021               1         0.38673        0.099188
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0042508     7.3921e-005      0.00019668

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.36          305.92
v  Yplus               0          2.9559         0.62775         0.48089


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4426               2          1.1833          1.0757


 INSTANT    0.334000000E-02   TIME STEP NUMBER             334
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924246E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17308E-01 0.47026E+01
   Friction velocity        uk    :  0.17308E-01 0.46986E+01
   Dimensionless distance   yplus :  0.11735E-01 0.29561E+01
   Friction thermal sca.    tstar :  0.17784E-01 0.14742E+03
   Rough dim-less th. sca.  tplus :  0.83132E-02 0.20941E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26695E+00       9   0.54650E-05   0.33049E+01 0.28608E+02 
c  Velocity[X]                                      0.10553E+01 
c  Velocity[Y]                                      0.11104E+01 
c  Velocity[Z]                                      0.11392E+01 
c  Pressure     0.11245E-04      18   0.18948E-03   0.11214E-01 0.16146E+02 
c  k            0.57703E-02      12   0.12954E-04   0.29398E-01 0.87946E+02 
c  omega        0.27923E+07       1   0.12582E-06   0.12931E+08 0.54426E+00 
c  TempK        0.95003E+04       7   0.36584E-05   0.13582E+03 0.37943E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.2714e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.261          19.007        0.008256      -0.0075842
v  Velocity[Y]             -15.473          14.839        0.076616         0.10893
v  Velocity[Z]             -25.881            14.7         -1.6278        -0.50053
v  ǁVelocityǁ         0.00092114          26.058          7.7089          6.6787
v  Pressure                -547.61          210.82          33.619          37.462
v  k                   1.0143e-010          8.2106         0.10295         0.16109
v  omega                    57.504     2.7329e+008     1.2911e+006           76730
v  TempK                    298.15          363.17          327.78          330.43
v  TurbVisc            2.5414e-018      0.00038176     2.3933e-005     7.0504e-005
v  CourantNb            9.326e-005          1.3753         0.79665         0.97655
v  FourierNb             0.0037019               1         0.38677        0.099422
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0042196     7.3903e-005      0.00019664

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.37          305.92
v  Yplus               0          2.9561         0.62797          0.4812


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.8771               2          1.1834           1.076


 INSTANT    0.335000000E-02   TIME STEP NUMBER             335
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924453E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17398E-01 0.47028E+01
   Friction velocity        uk    :  0.17398E-01 0.46988E+01
   Dimensionless distance   yplus :  0.11796E-01 0.29562E+01
   Friction thermal sca.    tstar :  0.18887E-01 0.14666E+03
   Rough dim-less th. sca.  tplus :  0.83563E-02 0.20942E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26713E+00       9   0.53881E-05   0.32253E+01 0.28293E+02 
c  Velocity[X]                                      0.10293E+01 
c  Velocity[Y]                                      0.10900E+01 
c  Velocity[Z]                                      0.11060E+01 
c  Pressure     0.11559E-04      18   0.18897E-03   0.11524E-01 0.15497E+02 
c  k            0.58067E-02      12   0.12876E-04   0.29224E-01 0.87073E+02 
c  omega        0.27923E+07       1   0.12604E-06   0.15061E+08 0.58547E+00 
c  TempK        0.95061E+04       7   0.36343E-05   0.13423E+03 0.37794E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.2587e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.261          19.014       0.0082494      -0.0076011
v  Velocity[Y]             -15.576          14.849        0.076915         0.10933
v  Velocity[Z]             -25.884          14.285         -1.6286        -0.50088
v  ǁVelocityǁ         0.00092406          26.062          7.7105          6.6806
v  Pressure                -547.78           210.9          33.696          37.525
v  k                   1.0144e-010          8.1874          0.1033         0.16216
v  omega                    57.504     2.7329e+008     1.2911e+006           76732
v  TempK                    298.15          363.17          327.82          330.51
v  TurbVisc            2.5417e-018      0.00038462     2.4032e-005     7.0976e-005
v  CourantNb           9.3584e-005          1.3777         0.79671         0.97656
v  FourierNb             0.0037017               1         0.38681        0.099656
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0041914     7.3886e-005       0.0001966

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.37          305.92
v  Yplus               0          2.9562         0.62818          0.4815


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.32156               2          1.1835          1.0762


 INSTANT    0.336000000E-02   TIME STEP NUMBER             336
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924401E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17496E-01 0.47030E+01
   Friction velocity        uk    :  0.17496E-01 0.46989E+01
   Dimensionless distance   yplus :  0.11863E-01 0.29564E+01
   Friction thermal sca.    tstar :  0.20054E-01 0.14583E+03
   Rough dim-less th. sca.  tplus :  0.84035E-02 0.20944E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26731E+00       9   0.53198E-05   0.31494E+01 0.28001E+02 
c  Velocity[X]                                      0.10056E+01 
c  Velocity[Y]                                      0.10712E+01 
c  Velocity[Z]                                      0.10726E+01 
c  Pressure     0.10886E-04      18   0.18641E-03   0.10851E-01 0.15090E+02 
c  k            0.58433E-02      12   0.12877E-04   0.29073E-01 0.86230E+02 
c  omega        0.27923E+07       1   0.12723E-06   0.22764E+08 0.71565E+00 
c  TempK        0.95119E+04       7   0.36093E-05   0.13261E+03 0.37643E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.2461e-007                             3


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.261           19.02       0.0082478      -0.0076198
v  Velocity[Y]             -15.616          14.858        0.077215         0.10974
v  Velocity[Z]             -25.888          13.959         -1.6294        -0.50123
v  ǁVelocityǁ         0.00092724          26.065          7.7121          6.6825
v  Pressure                -547.94          210.98          33.771          37.584
v  k                   1.0145e-010          8.1643         0.10366         0.16323
v  omega                    57.504     2.7329e+008     1.2911e+006           76735
v  TempK                    298.15          363.17          327.87          330.58
v  TurbVisc            2.5419e-018      0.00038744     2.4131e-005     7.1449e-005
v  CourantNb            9.389e-005            1.38         0.79677         0.97657
v  FourierNb             0.0037014               1         0.38685         0.09989
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0041654      7.387e-005      0.00019656

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.38          305.92
v  Yplus               0          2.9564         0.62839          0.4818


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82184               2          1.1836          1.0765


 INSTANT    0.337000000E-02   TIME STEP NUMBER             337
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924262E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17610E-01 0.47031E+01
   Friction velocity        uk    :  0.17610E-01 0.46991E+01
   Dimensionless distance   yplus :  0.11940E-01 0.29566E+01
   Friction thermal sca.    tstar :  0.21282E-01 0.14489E+03
   Rough dim-less th. sca.  tplus :  0.84582E-02 0.20945E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26749E+00       9   0.52448E-05   0.30650E+01 0.27697E+02 
c  Velocity[X]                                      0.98093E+00 
c  Velocity[Y]                                      0.10535E+01 
c  Velocity[Z]                                      0.10306E+01 
c  Pressure     0.10735E-04      18   0.18609E-03   0.10697E-01 0.15223E+02 
c  k            0.58800E-02      12   0.12766E-04   0.28930E-01 0.85416E+02 
c  omega        0.27923E+07       1   0.12423E-06   0.12528E+08 0.53994E+00 
c  TempK        0.95175E+04       7   0.35845E-05   0.13098E+03 0.37491E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.2342e-007                             4


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.261          19.026       0.0082435        -0.00764
v  Velocity[Y]             -15.528          14.868        0.077518         0.11015
v  Velocity[Z]             -25.892          13.708         -1.6302        -0.50158
v  ǁVelocityǁ         0.00093041          26.069          7.7137          6.6844
v  Pressure                -548.09          211.06          33.847          37.647
v  k                   1.0146e-010          8.1414         0.10401         0.16431
v  omega                    57.505     2.7329e+008     1.2911e+006           76737
v  TempK                    298.15          363.17          327.92          330.66
v  TurbVisc            2.5422e-018      0.00039023      2.423e-005     7.1923e-005
v  CourantNb           9.4222e-005          1.3823         0.79682         0.97658
v  FourierNb             0.0037013               1         0.38689         0.10012
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.004141     7.3854e-005      0.00019652

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.39          305.93
v  Yplus               0          2.9566         0.62859         0.48209


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56278               2          1.1837          1.0767


 INSTANT    0.338000000E-02   TIME STEP NUMBER             338
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924336E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17732E-01 0.47033E+01
   Friction velocity        uk    :  0.17732E-01 0.46993E+01
   Dimensionless distance   yplus :  0.12023E-01 0.29568E+01
   Friction thermal sca.    tstar :  0.22578E-01 0.14389E+03
   Rough dim-less th. sca.  tplus :  0.85168E-02 0.20946E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26766E+00       9   0.51728E-05   0.29825E+01 0.27351E+02 
c  Velocity[X]                                      0.95675E+00 
c  Velocity[Y]                                      0.10294E+01 
c  Velocity[Z]                                      0.99632E+00 
c  Pressure     0.10292E-04      18   0.18519E-03   0.10253E-01 0.14489E+02 
c  k            0.59170E-02      12   0.12690E-04   0.28795E-01 0.84640E+02 
c  omega        0.27923E+07       1   0.12264E-06   0.84102E+07 0.44715E+00 
c  TempK        0.95232E+04       7   0.35592E-05   0.12934E+03 0.37338E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.2223e-007                             4


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.26          19.032       0.0082417      -0.0076633
v  Velocity[Y]             -15.474          14.878        0.077821         0.11056
v  Velocity[Z]             -25.896          13.649          -1.631        -0.50192
v  ǁVelocityǁ         0.00093385          26.073          7.7153          6.6862
v  Pressure                -548.24          211.14          33.918          37.703
v  k                   1.0147e-010          8.1187         0.10436         0.16538
v  omega                    57.505     2.7329e+008     1.2911e+006           76739
v  TempK                    298.16          363.17          327.96          330.73
v  TurbVisc            2.5424e-018      0.00039298     2.4329e-005     7.2398e-005
v  CourantNb           9.4548e-005          1.3846         0.79688         0.97658
v  FourierNb             0.0037011               1         0.38694         0.10036
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0041184     7.3838e-005      0.00019649

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           304.4          305.93
v  Yplus               0          2.9568         0.62879         0.48238


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68457               2          1.1838          1.0769


 INSTANT    0.339000000E-02   TIME STEP NUMBER             339
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924427E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17871E-01 0.47034E+01
   Friction velocity        uk    :  0.17871E-01 0.46994E+01
   Dimensionless distance   yplus :  0.12117E-01 0.29570E+01
   Friction thermal sca.    tstar :  0.23946E-01 0.14350E+03
   Rough dim-less th. sca.  tplus :  0.85838E-02 0.20948E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26784E+00       9   0.51001E-05   0.29071E+01 0.27054E+02 
c  Velocity[X]                                      0.93402E+00 
c  Velocity[Y]                                      0.10096E+01 
c  Velocity[Z]                                      0.96347E+00 
c  Pressure     0.10194E-04      18   0.18415E-03   0.10154E-01 0.14009E+02 
c  k            0.59541E-02      12   0.12629E-04   0.28644E-01 0.83881E+02 
c  omega        0.27923E+07       1   0.12203E-06   0.78316E+07 0.43651E+00 
c  TempK        0.95287E+04       7   0.35334E-05   0.12767E+03 0.37183E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.2102e-007                             4


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.26          19.038       0.0082399      -0.0076886
v  Velocity[Y]             -15.472          14.888        0.078127         0.11097
v  Velocity[Z]               -25.9           13.47         -1.6318        -0.50227
v  ǁVelocityǁ         0.00093695          26.077          7.7168          6.6881
v  Pressure                -548.38          211.21          33.985          37.756
v  k                   1.0148e-010          8.0961         0.10472         0.16646
v  omega                    57.505     2.7329e+008     1.2911e+006           76742
v  TempK                    298.16          363.17          328.01          330.81
v  TurbVisc            2.5427e-018       0.0003957     2.4428e-005     7.2874e-005
v  CourantNb           9.4894e-005          1.3869         0.79693         0.97659
v  FourierNb             0.0037009               1         0.38698         0.10059
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0040978     7.3823e-005      0.00019645

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.41          305.93
v  Yplus               0           2.957         0.62899         0.48267


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.656               2          1.1839          1.0772


 INSTANT    0.340000000E-02   TIME STEP NUMBER             340
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924413E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18003E-01 0.47036E+01
   Friction velocity        uk    :  0.18003E-01 0.46995E+01
   Dimensionless distance   yplus :  0.12206E-01 0.29572E+01
   Friction thermal sca.    tstar :  0.25382E-01 0.14379E+03
   Rough dim-less th. sca.  tplus :  0.86470E-02 0.20949E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26801E+00       9   0.50199E-05   0.28373E+01 0.26791E+02 
c  Velocity[X]                                      0.91255E+00 
c  Velocity[Y]                                      0.99035E+00 
c  Velocity[Z]                                      0.93435E+00 
c  Pressure     0.10107E-04      18   0.18350E-03   0.10064E-01 0.14575E+02 
c  k            0.59914E-02      11   0.13373E-04   0.28486E-01 0.83118E+02 
c  omega        0.27922E+07       1   0.12317E-06   0.11778E+08 0.52607E+00 
c  TempK        0.95342E+04       7   0.35071E-05   0.12600E+03 0.37026E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.1979e-007                             4


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.26          19.044       0.0082385      -0.0077163
v  Velocity[Y]             -15.496          14.898        0.078439         0.11138
v  Velocity[Z]             -25.903          13.406         -1.6326        -0.50261
v  ǁVelocityǁ         0.00094085           26.08          7.7183          6.6898
v  Pressure                -548.49          211.28          34.057          37.814
v  k                   1.0149e-010          8.0739         0.10507         0.16754
v  omega                    57.506     2.7329e+008     1.2911e+006           76744
v  TempK                    298.16          363.17          328.06          330.88
v  TurbVisc            2.5429e-018      0.00039836     2.4527e-005      7.335e-005
v  CourantNb             9.52e-005          1.3893         0.79698          0.9766
v  FourierNb             0.0037007               1         0.38703         0.10083
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.004079     7.3808e-005      0.00019642

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.41          305.94
v  Yplus               0          2.9572         0.62919         0.48295


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66392               2           1.184          1.0774


 INSTANT    0.341000000E-02   TIME STEP NUMBER             341
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924362E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18176E-01 0.47037E+01
   Friction velocity        uk    :  0.18176E-01 0.46997E+01
   Dimensionless distance   yplus :  0.12323E-01 0.29574E+01
   Friction thermal sca.    tstar :  0.26887E-01 0.14403E+03
   Rough dim-less th. sca.  tplus :  0.87299E-02 0.20950E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26818E+00       9   0.49516E-05   0.27728E+01 0.26574E+02 
c  Velocity[X]                                      0.89246E+00 
c  Velocity[Y]                                      0.97499E+00 
c  Velocity[Z]                                      0.90536E+00 
c  Pressure     0.99712E-05      18   0.18045E-03   0.99270E-02 0.14810E+02 
c  k            0.60288E-02      11   0.13308E-04   0.28334E-01 0.82364E+02 
c  omega        0.27922E+07       1   0.12560E-06   0.24022E+08 0.73995E+00 
c  TempK        0.95397E+04       7   0.34805E-05   0.12432E+03 0.36868E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.1853e-007                             4


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.26           19.05       0.0082388      -0.0077456
v  Velocity[Y]               -15.6          14.908         0.07875         0.11179
v  Velocity[Z]             -25.907           13.26         -1.6334        -0.50295
v  ǁVelocityǁ         0.00094416          26.083          7.7198          6.6916
v  Pressure                -548.58          211.36          34.131          37.874
v  k                    1.015e-010          8.0519         0.10542         0.16862
v  omega                    57.506     2.7328e+008     1.2912e+006           76746
v  TempK                    298.16          363.17           328.1          330.95
v  TurbVisc            2.5431e-018      0.00040098     2.4626e-005     7.3827e-005
v  CourantNb            9.558e-005          1.3917         0.79703         0.97661
v  FourierNb             0.0037005               1         0.38708         0.10106
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0040617     7.3794e-005      0.00019638

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.42          305.94
v  Yplus               0          2.9574         0.62939         0.48323


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60818               2          1.1841          1.0777


 INSTANT    0.342000000E-02   TIME STEP NUMBER             342
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924387E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18326E-01 0.47038E+01
   Friction velocity        uk    :  0.18326E-01 0.46998E+01
   Dimensionless distance   yplus :  0.12425E-01 0.29575E+01
   Friction thermal sca.    tstar :  0.28473E-01 0.14426E+03
   Rough dim-less th. sca.  tplus :  0.88023E-02 0.20951E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26834E+00       9   0.48962E-05   0.27030E+01 0.26282E+02 
c  Velocity[X]                                      0.87206E+00 
c  Velocity[Y]                                      0.95523E+00 
c  Velocity[Z]                                      0.87571E+00 
c  Pressure     0.10089E-04      18   0.17984E-03   0.10042E-01 0.14111E+02 
c  k            0.60663E-02      11   0.13256E-04   0.28171E-01 0.81606E+02 
c  omega        0.27922E+07       1   0.12545E-06   0.25543E+08 0.76361E+00 
c  TempK        0.95451E+04       7   0.34538E-05   0.12263E+03 0.36709E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.1729e-007                             4


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.259          19.056       0.0082417      -0.0077756
v  Velocity[Y]              -15.64          14.918         0.07906          0.1122
v  Velocity[Z]              -25.91          13.233         -1.6341        -0.50328
v  ǁVelocityǁ         0.00094796          26.086          7.7212          6.6933
v  Pressure                -548.65          211.43          34.201           37.93
v  k                   1.0151e-010          8.0303         0.10577          0.1697
v  omega                    57.507     2.7328e+008     1.2912e+006           76749
v  TempK                    298.16          363.17          328.15          331.03
v  TurbVisc            2.5434e-018      0.00040354     2.4726e-005     7.4304e-005
v  CourantNb           9.5896e-005          1.3941         0.79708         0.97661
v  FourierNb             0.0037003               1         0.38712         0.10129
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0040456     7.3779e-005      0.00019635

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.43          305.94
v  Yplus               0          2.9575         0.62958         0.48351


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85329               2          1.1842          1.0779


 INSTANT    0.343000000E-02   TIME STEP NUMBER             343
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924353E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18487E-01 0.47039E+01
   Friction velocity        uk    :  0.18487E-01 0.46999E+01
   Dimensionless distance   yplus :  0.12534E-01 0.29577E+01
   Friction thermal sca.    tstar :  0.30150E-01 0.14448E+03
   Rough dim-less th. sca.  tplus :  0.88795E-02 0.20952E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26851E+00       9   0.48334E-05   0.26381E+01 0.25995E+02 
c  Velocity[X]                                      0.85108E+00 
c  Velocity[Y]                                      0.93665E+00 
c  Velocity[Z]                                      0.85039E+00 
c  Pressure     0.10529E-04      18   0.18143E-03   0.10478E-01 0.14062E+02 
c  k            0.61040E-02      11   0.13256E-04   0.28012E-01 0.80863E+02 
c  omega        0.27922E+07       1   0.12147E-06   0.12650E+08 0.55019E+00 
c  TempK        0.95504E+04       7   0.34268E-05   0.12093E+03 0.36548E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      7.161e-007                             4


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.259          19.061       0.0082411      -0.0078057
v  Velocity[Y]             -15.551          14.928        0.079373         0.11262
v  Velocity[Z]             -25.913          13.118         -1.6349        -0.50362
v  ǁVelocityǁ         0.00095152          26.089          7.7226           6.695
v  Pressure                 -548.7           211.5          34.271          37.986
v  k                   1.0152e-010           8.009         0.10612         0.17078
v  omega                    57.507     2.7328e+008     1.2912e+006           76751
v  TempK                    298.16          363.17           328.2           331.1
v  TurbVisc            2.5436e-018      0.00040605     2.4825e-005     7.4782e-005
v  CourantNb           9.6252e-005          1.3964         0.79712         0.97662
v  FourierNb             0.0037002               1         0.38717         0.10153
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0040307     7.3765e-005      0.00019632

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.44          305.95
v  Yplus               0          2.9577         0.62976         0.48378


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52315               2          1.1843          1.0781


 INSTANT    0.344000000E-02   TIME STEP NUMBER             344
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924352E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18461E-01 0.47040E+01
   Friction velocity        uk    :  0.18461E-01 0.47000E+01
   Dimensionless distance   yplus :  0.12517E-01 0.29578E+01
   Friction thermal sca.    tstar :  0.31922E-01 0.14468E+03
   Rough dim-less th. sca.  tplus :  0.88671E-02 0.20953E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26867E+00       9   0.47650E-05   0.25673E+01 0.25671E+02 
c  Velocity[X]                                      0.83080E+00 
c  Velocity[Y]                                      0.91336E+00 
c  Velocity[Z]                                      0.82313E+00 
c  Pressure     0.10114E-04      18   0.18008E-03   0.10063E-01 0.13972E+02 
c  k            0.61419E-02      11   0.13228E-04   0.27880E-01 0.80191E+02 
c  omega        0.27922E+07       1   0.11942E-06   0.78886E+07 0.44362E+00 
c  TempK        0.95557E+04       7   0.33998E-05   0.11922E+03 0.36385E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.1492e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.259          19.067       0.0082428      -0.0078364
v  Velocity[Y]             -15.497          14.939        0.079685         0.11303
v  Velocity[Z]             -25.917          13.102         -1.6356        -0.50394
v  ǁVelocityǁ         0.00095586          26.093           7.724          6.6967
v  Pressure                -548.72          211.58           34.34          38.041
v  k                   1.0152e-010          7.9881         0.10646         0.17186
v  omega                    57.507     2.7328e+008     1.2912e+006           76753
v  TempK                    298.16          363.17          328.24          331.17
v  TurbVisc            2.5438e-018      0.00040921     2.4924e-005      7.526e-005
v  CourantNb           9.6577e-005          1.3988         0.79717         0.97662
v  FourierNb             0.0037001               1         0.38722         0.10176
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0040169     7.3751e-005      0.00019629

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.44          305.95
v  Yplus               0          2.9578         0.62994         0.48404


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.95285               2          1.1844          1.0784


 INSTANT    0.345000000E-02   TIME STEP NUMBER             345
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924158E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18438E-01 0.47041E+01
   Friction velocity        uk    :  0.18438E-01 0.47001E+01
   Dimensionless distance   yplus :  0.12501E-01 0.29580E+01
   Friction thermal sca.    tstar :  0.33788E-01 0.14485E+03
   Rough dim-less th. sca.  tplus :  0.88561E-02 0.20955E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26883E+00       9   0.47065E-05   0.24965E+01 0.25387E+02 
c  Velocity[X]                                      0.81144E+00 
c  Velocity[Y]                                      0.89383E+00 
c  Velocity[Z]                                      0.79121E+00 
c  Pressure     0.98788E-05      18   0.17770E-03   0.98273E-02 0.14240E+02 
c  k            0.61799E-02      11   0.13138E-04   0.27800E-01 0.79649E+02 
c  omega        0.27922E+07       1   0.11860E-06   0.74034E+07 0.43388E+00 
c  TempK        0.95610E+04       7   0.33730E-05   0.11752E+03 0.36220E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.1372e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.259          19.072       0.0082458      -0.0078667
v  Velocity[Y]             -15.495          14.949            0.08         0.11345
v  Velocity[Z]              -25.92          12.989         -1.6364        -0.50427
v  ǁVelocityǁ          0.0009598          26.096          7.7253          6.6984
v  Pressure                -548.72          211.66          34.412            38.1
v  k                   1.0153e-010          7.9677         0.10681         0.17295
v  omega                    57.507     2.7328e+008     1.2912e+006           76755
v  TempK                    298.16          363.17          328.29          331.24
v  TurbVisc             2.544e-018      0.00041305     2.5024e-005     7.5738e-005
v  CourantNb           9.6974e-005          1.4011         0.79721         0.97663
v  FourierNb             0.0036999               1         0.38727         0.10199
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0040042     7.3737e-005      0.00019626

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.45          305.95
v  Yplus               0           2.958         0.63013          0.4843


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69624               2          1.1845          1.0786


 INSTANT    0.346000000E-02   TIME STEP NUMBER             346
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924203E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18417E-01 0.47042E+01
   Friction velocity        uk    :  0.18417E-01 0.47001E+01
   Dimensionless distance   yplus :  0.12487E-01 0.29582E+01
   Friction thermal sca.    tstar :  0.35768E-01 0.14502E+03
   Rough dim-less th. sca.  tplus :  0.88459E-02 0.20956E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26898E+00       9   0.46566E-05   0.24339E+01 0.25122E+02 
c  Velocity[X]                                      0.79393E+00 
c  Velocity[Y]                                      0.87484E+00 
c  Velocity[Z]                                      0.76517E+00 
c  Pressure     0.99312E-05      18   0.17600E-03   0.98778E-02 0.13395E+02 
c  k            0.62180E-02      11   0.12997E-04   0.27677E-01 0.79019E+02 
c  omega        0.27922E+07       1   0.11833E-06   0.87907E+07 0.46787E+00 
c  TempK        0.95661E+04       7   0.33461E-05   0.11581E+03 0.36054E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.1249e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258          19.077       0.0082499      -0.0078983
v  Velocity[Y]             -15.519           14.96        0.080317         0.11387
v  Velocity[Z]             -25.923           12.97         -1.6371        -0.50459
v  ǁVelocityǁ         0.00096419          26.099          7.7266             6.7
v  Pressure                -548.69          211.73          34.478          38.153
v  k                   1.0154e-010          7.9477         0.10716         0.17403
v  omega                    57.508     2.7328e+008     1.2912e+006           76758
v  TempK                    298.16          363.17          328.33          331.31
v  TurbVisc            2.5443e-018      0.00041672     2.5123e-005     7.6217e-005
v  CourantNb           9.7325e-005          1.4035         0.79725         0.97664
v  FourierNb             0.0036998               1         0.38732         0.10223
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039925     7.3723e-005      0.00019623

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.46          305.96
v  Yplus               0          2.9582         0.63031         0.48456


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75812               2          1.1846          1.0789


 INSTANT    0.347000000E-02   TIME STEP NUMBER             347
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924213E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18399E-01 0.47042E+01
   Friction velocity        uk    :  0.18399E-01 0.47002E+01
   Dimensionless distance   yplus :  0.12475E-01 0.29583E+01
   Friction thermal sca.    tstar :  0.37863E-01 0.14516E+03
   Rough dim-less th. sca.  tplus :  0.88374E-02 0.20957E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26914E+00       9   0.46081E-05   0.23812E+01 0.24921E+02 
c  Velocity[X]                                      0.77781E+00 
c  Velocity[Y]                                      0.85725E+00 
c  Velocity[Z]                                      0.74614E+00 
c  Pressure     0.10359E-04      18   0.17619E-03   0.10302E-01 0.15367E+02 
c  k            0.62563E-02      11   0.12917E-04   0.27535E-01 0.78358E+02 
c  omega        0.27922E+07       1   0.12037E-06   0.16346E+08 0.61825E+00 
c  TempK        0.95713E+04       7   0.33193E-05   0.11411E+03 0.35886E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.1125e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258          19.083       0.0082523      -0.0079307
v  Velocity[Y]             -15.623           14.97        0.080639         0.11429
v  Velocity[Z]             -25.926          12.861         -1.6378        -0.50491
v  ǁVelocityǁ         0.00096822          26.102          7.7279          6.7016
v  Pressure                -548.63          211.81           34.56          38.221
v  k                   1.0155e-010          7.9283          0.1075         0.17512
v  omega                    57.508     2.7328e+008     1.2912e+006           76760
v  TempK                    298.16          363.17          328.38          331.38
v  TurbVisc            2.5445e-018       0.0004202     2.5222e-005     7.6696e-005
v  CourantNb            9.771e-005           1.406         0.79729         0.97664
v  FourierNb             0.0036996               1         0.38737         0.10246
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039817     7.3709e-005       0.0001962

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.47          305.96
v  Yplus               0          2.9583         0.63048         0.48481


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52178               2          1.1847          1.0791


 INSTANT    0.348000000E-02   TIME STEP NUMBER             348
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924447E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18383E-01 0.47043E+01
   Friction velocity        uk    :  0.18383E-01 0.47003E+01
   Dimensionless distance   yplus :  0.12464E-01 0.29584E+01
   Friction thermal sca.    tstar :  0.40083E-01 0.14529E+03
   Rough dim-less th. sca.  tplus :  0.88294E-02 0.20958E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26929E+00       9   0.45601E-05   0.23354E+01 0.24753E+02 
c  Velocity[X]                                      0.76409E+00 
c  Velocity[Y]                                      0.84428E+00 
c  Velocity[Z]                                      0.72703E+00 
c  Pressure     0.10447E-04      18   0.17435E-03   0.10387E-01 0.12551E+02 
c  k            0.62947E-02      11   0.12837E-04   0.27387E-01 0.77681E+02 
c  omega        0.27922E+07       1   0.12188E-06   0.27119E+08 0.78964E+00 
c  TempK        0.95763E+04       7   0.32925E-05   0.11242E+03 0.35718E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.1001e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258          19.088       0.0082581      -0.0079649
v  Velocity[Y]             -15.663          14.981        0.080957         0.11471
v  Velocity[Z]             -25.929          12.847         -1.6385        -0.50523
v  ǁVelocityǁ         0.00097272          26.105          7.7292          6.7032
v  Pressure                -548.56          211.88          34.618          38.266
v  k                   1.0156e-010          7.9093         0.10785          0.1762
v  omega                    57.508     2.7327e+008     1.2912e+006           76762
v  TempK                    298.16          363.17          328.43          331.45
v  TurbVisc            2.5447e-018      0.00042351     2.5321e-005     7.7174e-005
v  CourantNb           9.8056e-005          1.4084         0.79733         0.97665
v  FourierNb             0.0036995               1         0.38742         0.10269
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039717     7.3695e-005      0.00019617

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.47          305.96
v  Yplus               0          2.9584         0.63065         0.48506


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67813               2          1.1848          1.0793


 INSTANT    0.349000000E-02   TIME STEP NUMBER             349
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924313E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18367E-01 0.47044E+01
   Friction velocity        uk    :  0.18367E-01 0.47003E+01
   Dimensionless distance   yplus :  0.12453E-01 0.29586E+01
   Friction thermal sca.    tstar :  0.42437E-01 0.14541E+03
   Rough dim-less th. sca.  tplus :  0.88218E-02 0.20959E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26944E+00       9   0.45047E-05   0.22683E+01 0.24453E+02 
c  Velocity[X]                                      0.74711E+00 
c  Velocity[Y]                                      0.82548E+00 
c  Velocity[Z]                                      0.69569E+00 
c  Pressure     0.10184E-04      18   0.17460E-03   0.10124E-01 0.12397E+02 
c  k            0.63332E-02      11   0.12743E-04   0.27263E-01 0.77039E+02 
c  omega        0.27922E+07       1   0.11807E-06   0.15845E+08 0.61920E+00 
c  TempK        0.95814E+04       7   0.32660E-05   0.11074E+03 0.35549E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.0882e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258          19.093       0.0082597      -0.0080001
v  Velocity[Y]             -15.574          14.991         0.08128         0.11513
v  Velocity[Z]             -25.932          12.747         -1.6392        -0.50554
v  ǁVelocityǁ         0.00097712          26.108          7.7304          6.7047
v  Pressure                -548.47          211.93          34.677          38.312
v  k                   1.0157e-010          7.8908         0.10819         0.17728
v  omega                    57.509     2.7327e+008     1.2912e+006           76764
v  TempK                    298.16          363.17          328.47          331.52
v  TurbVisc            2.5449e-018      0.00042662      2.542e-005     7.7653e-005
v  CourantNb           9.8436e-005          1.4108         0.79737         0.97665
v  FourierNb             0.0036993               1         0.38747         0.10292
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039624     7.3681e-005      0.00019614

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.48          305.97
v  Yplus               0          2.9586         0.63082          0.4853


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69235               2          1.1848          1.0796


 INSTANT    0.350000000E-02   TIME STEP NUMBER             350
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924155E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18356E-01 0.47044E+01
   Friction velocity        uk    :  0.18356E-01 0.47004E+01
   Dimensionless distance   yplus :  0.12446E-01 0.29587E+01
   Friction thermal sca.    tstar :  0.44932E-01 0.14549E+03
   Rough dim-less th. sca.  tplus :  0.88168E-02 0.20960E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26959E+00       9   0.44526E-05   0.22112E+01 0.24149E+02 
c  Velocity[X]                                      0.73288E+00 
c  Velocity[Y]                                      0.80293E+00 
c  Velocity[Z]                                      0.67543E+00 
c  Pressure     0.10338E-04      18   0.17321E-03   0.10274E-01 0.13293E+02 
c  k            0.63719E-02      11   0.12650E-04   0.27155E-01 0.76430E+02 
c  omega        0.27922E+07       1   0.11455E-06   0.75863E+07 0.44657E+00 
c  TempK        0.95863E+04       7   0.32405E-05   0.10907E+03 0.35379E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.0764e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.098       0.0082605      -0.0080367
v  Velocity[Y]              -15.52          15.002          0.0816         0.11556
v  Velocity[Z]             -25.935          12.742         -1.6399        -0.50584
v  ǁVelocityǁ         0.00097906          26.111          7.7316          6.7063
v  Pressure                -548.36          212.01          34.745          38.367
v  k                   1.0157e-010           7.873         0.10853         0.17837
v  omega                    57.509     2.7327e+008     1.2912e+006           76766
v  TempK                    298.16          363.17          328.52          331.59
v  TurbVisc            2.5451e-018      0.00042954     2.5519e-005     7.8132e-005
v  CourantNb           9.8804e-005          1.4131          0.7974         0.97666
v  FourierNb             0.0036992               1         0.38752         0.10315
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039539     7.3667e-005      0.00019611

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.49          305.97
v  Yplus               0          2.9587         0.63098         0.48554


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4443               2          1.1849          1.0798


 INSTANT    0.351000000E-02   TIME STEP NUMBER             351
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924262E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18349E-01 0.47045E+01
   Friction velocity        uk    :  0.18349E-01 0.47004E+01
   Dimensionless distance   yplus :  0.12441E-01 0.29588E+01
   Friction thermal sca.    tstar :  0.47586E-01 0.14555E+03
   Rough dim-less th. sca.  tplus :  0.88133E-02 0.20961E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26973E+00       9   0.44049E-05   0.21601E+01 0.23915E+02 
c  Velocity[X]                                      0.71953E+00 
c  Velocity[Y]                                      0.78555E+00 
c  Velocity[Z]                                      0.65499E+00 
c  Pressure     0.10367E-04      17   0.16978E-03   0.10302E-01 0.12146E+02 
c  k            0.64106E-02      11   0.12557E-04   0.27041E-01 0.75842E+02 
c  omega        0.27922E+07       1   0.11328E-06   0.68067E+07 0.43205E+00 
c  TempK        0.95912E+04       7   0.32154E-05   0.10741E+03 0.35209E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.0646e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.103       0.0082631      -0.0080737
v  Velocity[Y]             -15.518          15.012        0.081921         0.11599
v  Velocity[Z]             -25.938          12.655         -1.6406        -0.50614
v  ǁVelocityǁ         0.00097794          26.114          7.7328          6.7078
v  Pressure                -548.24          212.07          34.802          38.412
v  k                   1.0158e-010          7.8557         0.10888         0.17945
v  omega                    57.509     2.7327e+008     1.2912e+006           76768
v  TempK                    298.16          363.17          328.56          331.66
v  TurbVisc            2.5453e-018      0.00043225     2.5618e-005     7.8611e-005
v  CourantNb           9.9191e-005          1.4155         0.79744         0.97666
v  FourierNb             0.0036991               1         0.38758         0.10338
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039463     7.3654e-005      0.00019608

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           304.5          305.97
v  Yplus               0          2.9588         0.63113         0.48577


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94294               2           1.185            1.08


 INSTANT    0.352000000E-02   TIME STEP NUMBER             352
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924261E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18340E-01 0.47045E+01
   Friction velocity        uk    :  0.18340E-01 0.47005E+01
   Dimensionless distance   yplus :  0.12435E-01 0.29590E+01
   Friction thermal sca.    tstar :  0.50409E-01 0.14562E+03
   Rough dim-less th. sca.  tplus :  0.88090E-02 0.20962E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26987E+00       9   0.43665E-05   0.21143E+01 0.23693E+02 
c  Velocity[X]                                      0.70798E+00 
c  Velocity[Y]                                      0.76864E+00 
c  Velocity[Z]                                      0.63769E+00 
c  Pressure     0.10706E-04      18   0.16923E-03   0.10636E-01 0.12682E+02 
c  k            0.64495E-02      11   0.12511E-04   0.26930E-01 0.75270E+02 
c  omega        0.27922E+07       1   0.11215E-06   0.66967E+07 0.42841E+00 
c  TempK        0.95961E+04       7   0.31907E-05   0.10577E+03 0.35038E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.0526e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.108       0.0082643       -0.008112
v  Velocity[Y]             -15.542          15.023        0.082243         0.11642
v  Velocity[Z]             -25.941          12.663         -1.6413        -0.50644
v  ǁVelocityǁ         0.00097679          26.117          7.7339          6.7093
v  Pressure                 -548.1          212.14          34.866          38.463
v  k                   1.0159e-010          7.8389         0.10922         0.18054
v  omega                     57.51     2.7327e+008     1.2912e+006           76770
v  TempK                    298.16          363.17          328.61          331.73
v  TurbVisc            2.5455e-018      0.00043612     2.5717e-005      7.909e-005
v  CourantNb            9.956e-005          1.4179         0.79747         0.97667
v  FourierNb              0.003699               1         0.38763         0.10361
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039393     7.3641e-005      0.00019605

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           304.5          305.97
v  Yplus               0           2.959         0.63129           0.486


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.33173               2          1.1851          1.0803


 INSTANT    0.353000000E-02   TIME STEP NUMBER             353
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924333E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18336E-01 0.47045E+01
   Friction velocity        uk    :  0.18336E-01 0.47005E+01
   Dimensionless distance   yplus :  0.12432E-01 0.29591E+01
   Friction thermal sca.    tstar :  0.53410E-01 0.14565E+03
   Rough dim-less th. sca.  tplus :  0.88070E-02 0.20963E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27001E+00       9   0.43168E-05   0.20709E+01 0.23511E+02 
c  Velocity[X]                                      0.69603E+00 
c  Velocity[Y]                                      0.75195E+00 
c  Velocity[Z]                                      0.62287E+00 
c  Pressure     0.10255E-04      18   0.16771E-03   0.10185E-01 0.12755E+02 
c  k            0.64886E-02      11   0.12487E-04   0.26825E-01 0.74713E+02 
c  omega        0.27922E+07       1   0.11274E-06   0.11388E+08 0.53191E+00 
c  TempK        0.96009E+04       7   0.31663E-05   0.10416E+03 0.34866E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.0402e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.113       0.0082653      -0.0081517
v  Velocity[Y]             -15.646          15.034        0.082565         0.11685
v  Velocity[Z]             -25.944           12.59         -1.6419        -0.50673
v  ǁVelocityǁ         0.00097586           26.12          7.7351          6.7107
v  Pressure                -547.94           212.2          34.929          38.513
v  k                    1.016e-010          7.8228         0.10956         0.18162
v  omega                     57.51     2.7327e+008     1.2912e+006           76772
v  TempK                    298.16          363.17          328.66           331.8
v  TurbVisc            2.5457e-018      0.00044029     2.5816e-005     7.9568e-005
v  CourantNb           9.9972e-005          1.4204          0.7975         0.97667
v  FourierNb             0.0036988               1         0.38768         0.10384
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0042225     7.3628e-005      0.00019602

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.51          305.98
v  Yplus               0          2.9591         0.63145         0.48622


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.8984          2.0021          1.1852          1.0805


 INSTANT    0.354000000E-02   TIME STEP NUMBER             354
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924189E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18330E-01 0.47046E+01
   Friction velocity        uk    :  0.18330E-01 0.47005E+01
   Dimensionless distance   yplus :  0.12428E-01 0.29593E+01
   Friction thermal sca.    tstar :  0.56596E-01 0.14570E+03
   Rough dim-less th. sca.  tplus :  0.88039E-02 0.20964E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27015E+00       9   0.42742E-05   0.20208E+01 0.23360E+02 
c  Velocity[X]                                      0.68437E+00 
c  Velocity[Y]                                      0.74100E+00 
c  Velocity[Z]                                      0.59544E+00 
c  Pressure     0.99822E-05      18   0.16443E-03   0.99125E-02 0.13598E+02 
c  k            0.65277E-02      11   0.12356E-04   0.26717E-01 0.74165E+02 
c  omega        0.27922E+07       1   0.11588E-06   0.26597E+08 0.78465E+00 
c  TempK        0.96057E+04       7   0.31430E-05   0.10256E+03 0.34695E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.0281e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.118        0.008268      -0.0081923
v  Velocity[Y]             -15.686          15.044        0.082889         0.11728
v  Velocity[Z]             -25.947          12.614         -1.6426        -0.50702
v  ǁVelocityǁ          0.0009748          26.122          7.7362          6.7122
v  Pressure                -547.76          212.28          35.001          38.572
v  k                    1.016e-010          7.8071          0.1099         0.18271
v  omega                     57.51     2.7326e+008     1.2912e+006           76774
v  TempK                    298.17          363.17           328.7          331.86
v  TurbVisc            2.5459e-018      0.00044431     2.5914e-005     8.0047e-005
v  CourantNb            0.00010034          1.4229         0.79753         0.97668
v  FourierNb             0.0036987               1         0.38774         0.10407
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0043682     7.3616e-005        0.000196

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.52          305.98
v  Yplus               0          2.9593          0.6316         0.48644


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60362          2.0046          1.1853          1.0807


 INSTANT    0.355000000E-02   TIME STEP NUMBER             355
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924208E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18329E-01 0.47046E+01
   Friction velocity        uk    :  0.18329E-01 0.47006E+01
   Dimensionless distance   yplus :  0.12427E-01 0.29594E+01
   Friction thermal sca.    tstar :  0.59984E-01 0.14571E+03
   Rough dim-less th. sca.  tplus :  0.88034E-02 0.20964E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27029E+00       9   0.42443E-05   0.19786E+01 0.23178E+02 
c  Velocity[X]                                      0.67491E+00 
c  Velocity[Y]                                      0.72784E+00 
c  Velocity[Z]                                      0.57585E+00 
c  Pressure     0.10348E-04      17   0.16331E-03   0.10274E-01 0.11895E+02 
c  k            0.65669E-02      11   0.12311E-04   0.26611E-01 0.73626E+02 
c  omega        0.27922E+07       1   0.11122E-06   0.14892E+08 0.60196E+00 
c  TempK        0.96104E+04       7   0.31206E-05   0.10099E+03 0.34523E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     7.0164e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.123       0.0082651      -0.0082343
v  Velocity[Y]             -15.597          15.055        0.083215         0.11772
v  Velocity[Z]              -25.95          12.558         -1.6432         -0.5073
v  ǁVelocityǁ         0.00097364          26.125          7.7372          6.7136
v  Pressure                -547.58          212.34           35.06          38.618
v  k                   1.0161e-010           7.792         0.11024         0.18379
v  omega                     57.51     2.7326e+008     1.2912e+006           76776
v  TempK                    298.17          363.17          328.75          331.93
v  TurbVisc             2.546e-018      0.00044812     2.6013e-005     8.0526e-005
v  CourantNb            0.00010073          1.4252         0.79755         0.97668
v  FourierNb             0.0036986               1          0.3878          0.1043
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044151     7.3604e-005      0.00019597

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.52          305.98
v  Yplus               0          2.9594         0.63174         0.48665


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63779          2.0071          1.1853           1.081


 INSTANT    0.356000000E-02   TIME STEP NUMBER             356
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924268E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18331E-01 0.47046E+01
   Friction velocity        uk    :  0.18331E-01 0.47006E+01
   Dimensionless distance   yplus :  0.12429E-01 0.29595E+01
   Friction thermal sca.    tstar :  0.63600E-01 0.14568E+03
   Rough dim-less th. sca.  tplus :  0.88046E-02 0.20965E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27042E+00       9   0.42233E-05   0.19320E+01 0.22893E+02 
c  Velocity[X]                                      0.66639E+00 
c  Velocity[Y]                                      0.70760E+00 
c  Velocity[Z]                                      0.55805E+00 
c  Pressure     0.10582E-04      17   0.16658E-03   0.10503E-01 0.11040E+02 
c  k            0.66063E-02      11   0.12214E-04   0.26512E-01 0.73101E+02 
c  omega        0.27922E+07       1   0.10843E-06   0.10372E+08 0.51242E+00 
c  TempK        0.96151E+04       7   0.30988E-05   0.99451E+02 0.34350E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      7.005e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.127       0.0082608      -0.0082774
v  Velocity[Y]             -15.543          15.066        0.083538         0.11816
v  Velocity[Z]             -25.952          12.601         -1.6439        -0.50757
v  ǁVelocityǁ         0.00097251          26.128          7.7383           6.715
v  Pressure                 -547.4           212.4          35.111          38.658
v  k                   1.0162e-010          7.7772         0.11058         0.18488
v  omega                    57.511     2.7326e+008     1.2912e+006           76778
v  TempK                    298.17          363.17          328.79             332
v  TurbVisc            2.5462e-018       0.0004517     2.6111e-005     8.1004e-005
v  CourantNb            0.00010109          1.4276         0.79758         0.97668
v  FourierNb             0.0036984               1         0.38785         0.10453
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044539     7.3591e-005      0.00019594

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.53          305.99
v  Yplus               0          2.9595         0.63188         0.48685


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63115          2.0095          1.1854          1.0812


 INSTANT    0.357000000E-02   TIME STEP NUMBER             357
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924161E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18334E-01 0.47046E+01
   Friction velocity        uk    :  0.18334E-01 0.47006E+01
   Dimensionless distance   yplus :  0.12431E-01 0.29596E+01
   Friction thermal sca.    tstar :  0.67520E-01 0.14566E+03
   Rough dim-less th. sca.  tplus :  0.88060E-02 0.20966E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27055E+00       9   0.41807E-05   0.18899E+01 0.22674E+02 
c  Velocity[X]                                      0.65691E+00 
c  Velocity[Y]                                      0.69146E+00 
c  Velocity[Z]                                      0.54151E+00 
c  Pressure     0.10600E-04      17   0.16470E-03   0.10520E-01 0.11291E+02 
c  k            0.66458E-02      11   0.12133E-04   0.26413E-01 0.72586E+02 
c  omega        0.27922E+07       1   0.10587E-06   0.62702E+07 0.41521E+00 
c  TempK        0.96197E+04       7   0.30777E-05   0.97935E+02 0.34178E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.9934e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.132       0.0082557      -0.0083207
v  Velocity[Y]             -15.541          15.077        0.083861          0.1186
v  Velocity[Z]             -25.955          12.565         -1.6445        -0.50784
v  ǁVelocityǁ         0.00097151           26.13          7.7393          6.7164
v  Pressure                 -547.2          212.46          35.166          38.701
v  k                   1.0162e-010          7.7629         0.11092         0.18596
v  omega                    57.511     2.7326e+008     1.2912e+006           76780
v  TempK                    298.17          363.17          328.84          332.07
v  TurbVisc            2.5464e-018       0.0004551      2.621e-005     8.1482e-005
v  CourantNb            0.00010152          1.4299          0.7976         0.97669
v  FourierNb             0.0036983               1         0.38791         0.10475
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044879     7.3579e-005      0.00019592

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.54          305.99
v  Yplus               0          2.9596         0.63202         0.48705


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66195          2.0119          1.1855          1.0814


 INSTANT    0.358000000E-02   TIME STEP NUMBER             358
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924204E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18339E-01 0.47046E+01
   Friction velocity        uk    :  0.18339E-01 0.47006E+01
   Dimensionless distance   yplus :  0.12434E-01 0.29598E+01
   Friction thermal sca.    tstar :  0.71602E-01 0.14562E+03
   Rough dim-less th. sca.  tplus :  0.88083E-02 0.20967E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27068E+00       9   0.41390E-05   0.18513E+01 0.22492E+02 
c  Velocity[X]                                      0.64843E+00 
c  Velocity[Y]                                      0.67701E+00 
c  Velocity[Z]                                      0.52586E+00 
c  Pressure     0.10527E-04      17   0.16144E-03   0.10445E-01 0.11299E+02 
c  k            0.66854E-02      11   0.12015E-04   0.26308E-01 0.72072E+02 
c  omega        0.27922E+07       1   0.10446E-06   0.59541E+07 0.40831E+00 
c  TempK        0.96243E+04       7   0.30573E-05   0.96446E+02 0.34005E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.9815e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.136        0.008251      -0.0083651
v  Velocity[Y]             -15.566          15.088        0.084184         0.11904
v  Velocity[Z]             -25.958           12.63         -1.6451         -0.5081
v  ǁVelocityǁ         0.00097052          26.133          7.7403          6.7177
v  Pressure                -546.98          212.52          35.222          38.745
v  k                   1.0163e-010           7.749         0.11126         0.18704
v  omega                    57.511     2.7326e+008     1.2912e+006           76782
v  TempK                    298.17          363.17          328.88          332.13
v  TurbVisc            2.5466e-018      0.00045832     2.6308e-005     8.1959e-005
v  CourantNb            0.00010189          1.4324         0.79763         0.97669
v  FourierNb             0.0036981               1         0.38797         0.10498
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045212     7.3567e-005      0.00019589

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.54          305.99
v  Yplus               0          2.9598         0.63216         0.48725


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48527          2.0144          1.1856          1.0817


 INSTANT    0.359000000E-02   TIME STEP NUMBER             359
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924284E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18345E-01 0.47046E+01
   Friction velocity        uk    :  0.18345E-01 0.47006E+01
   Dimensionless distance   yplus :  0.12438E-01 0.29599E+01
   Friction thermal sca.    tstar :  0.75978E-01 0.14557E+03
   Rough dim-less th. sca.  tplus :  0.88114E-02 0.20968E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27081E+00       9   0.41089E-05   0.18193E+01 0.22346E+02 
c  Velocity[X]                                      0.64139E+00 
c  Velocity[Y]                                      0.66313E+00 
c  Velocity[Z]                                      0.51479E+00 
c  Pressure     0.10606E-04      17   0.16036E-03   0.10522E-01 0.11366E+02 
c  k            0.67251E-02      11   0.11987E-04   0.26207E-01 0.71567E+02 
c  omega        0.27922E+07       1   0.10428E-06   0.85686E+07 0.47143E+00 
c  TempK        0.96288E+04       7   0.30375E-05   0.94985E+02 0.33832E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.9693e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.141       0.0082447      -0.0084107
v  Velocity[Y]              -15.67          15.099        0.084504         0.11948
v  Velocity[Z]             -25.961          12.614         -1.6457        -0.50835
v  ǁVelocityǁ         0.00096972          26.136          7.7413           6.719
v  Pressure                -546.75          212.58          35.277          38.788
v  k                   1.0164e-010          7.7353          0.1116         0.18813
v  omega                    57.512     2.7326e+008     1.2912e+006           76784
v  TempK                    298.17          363.17          328.93           332.2
v  TurbVisc            2.5467e-018      0.00046139     2.6406e-005     8.2437e-005
v  CourantNb             0.0001023          1.4349         0.79765          0.9767
v  FourierNb              0.003698               1         0.38803          0.1052
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045547     7.3555e-005      0.00019586

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.55          305.99
v  Yplus               0          2.9599         0.63229         0.48745


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43011          2.0169          1.1857          1.0819


 INSTANT    0.360000000E-02   TIME STEP NUMBER             360
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924290E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18348E-01 0.47046E+01
   Friction velocity        uk    :  0.18348E-01 0.47006E+01
   Dimensionless distance   yplus :  0.12440E-01 0.29601E+01
   Friction thermal sca.    tstar :  0.80661E-01 0.14554E+03
   Rough dim-less th. sca.  tplus :  0.88129E-02 0.20969E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27093E+00       9   0.40811E-05   0.17911E+01 0.22219E+02 
c  Velocity[X]                                      0.63472E+00 
c  Velocity[Y]                                      0.65207E+00 
c  Velocity[Z]                                      0.50432E+00 
c  Pressure     0.10382E-04      17   0.15884E-03   0.10298E-01 0.11125E+02 
c  k            0.67648E-02      11   0.11924E-04   0.26099E-01 0.71064E+02 
c  omega        0.27922E+07       1   0.10625E-06   0.20219E+08 0.69249E+00 
c  TempK        0.96333E+04       7   0.30181E-05   0.93554E+02 0.33659E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.9572e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.145       0.0082405      -0.0084585
v  Velocity[Y]             -15.711          15.109        0.084824         0.11992
v  Velocity[Z]             -25.964          12.702         -1.6462         -0.5086
v  ǁVelocityǁ         0.00096885          26.139          7.7422          6.7204
v  Pressure                 -546.5          212.64          35.331           38.83
v  k                   1.0164e-010          7.7218         0.11194         0.18921
v  omega                    57.512     2.7325e+008     1.2912e+006           76786
v  TempK                    298.17          363.17          328.97          332.26
v  TurbVisc            2.5469e-018      0.00046431     2.6504e-005     8.2913e-005
v  CourantNb            0.00010266          1.4374         0.79767          0.9767
v  FourierNb             0.0036979               1         0.38809         0.10543
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045893     7.3543e-005      0.00019584

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.56             306
v  Yplus               0          2.9601         0.63243         0.48764


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77441          2.0195          1.1858          1.0821


 INSTANT    0.361000000E-02   TIME STEP NUMBER             361
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924202E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18356E-01 0.47046E+01
   Friction velocity        uk    :  0.18356E-01 0.47006E+01
   Dimensionless distance   yplus :  0.12445E-01 0.29602E+01
   Friction thermal sca.    tstar :  0.85677E-01 0.14548E+03
   Rough dim-less th. sca.  tplus :  0.88165E-02 0.20970E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27105E+00       9   0.40505E-05   0.17557E+01 0.22079E+02 
c  Velocity[X]                                      0.62683E+00 
c  Velocity[Y]                                      0.64139E+00 
c  Velocity[Z]                                      0.48747E+00 
c  Pressure     0.10015E-04      17   0.15853E-03   0.99316E-02 0.11729E+02 
c  k            0.68047E-02      11   0.11916E-04   0.25992E-01 0.70564E+02 
c  omega        0.27922E+07       1   0.10318E-06   0.12895E+08 0.56603E+00 
c  TempK        0.96377E+04       7   0.29996E-05   0.92151E+02 0.33485E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.9457e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256           19.15       0.0082316      -0.0085079
v  Velocity[Y]             -15.621           15.12         0.08515         0.12036
v  Velocity[Z]             -25.967          12.707         -1.6468        -0.50884
v  ǁVelocityǁ         0.00096781          26.142          7.7432          6.7216
v  Pressure                -546.24           212.7          35.391          38.879
v  k                   1.0165e-010          7.7084         0.11228         0.19029
v  omega                    57.512     2.7325e+008     1.2912e+006           76787
v  TempK                    298.17          363.17          329.02          332.33
v  TurbVisc             2.547e-018      0.00046708     2.6602e-005     8.3389e-005
v  CourantNb            0.00010306          1.4397         0.79769          0.9767
v  FourierNb             0.0036977               1         0.38815         0.10565
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046332     7.3531e-005      0.00019581

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.56             306
v  Yplus               0          2.9602         0.63255         0.48782


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59227          2.0219          1.1858          1.0824


 INSTANT    0.362000000E-02   TIME STEP NUMBER             362
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924423E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18371E-01 0.47046E+01
   Friction velocity        uk    :  0.18371E-01 0.47006E+01
   Dimensionless distance   yplus :  0.12456E-01 0.29603E+01
   Friction thermal sca.    tstar :  0.91056E-01 0.14536E+03
   Rough dim-less th. sca.  tplus :  0.88237E-02 0.20971E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27117E+00       9   0.40223E-05   0.17203E+01 0.21905E+02 
c  Velocity[X]                                      0.61929E+00 
c  Velocity[Y]                                      0.62862E+00 
c  Velocity[Z]                                      0.47239E+00 
c  Pressure     0.98676E-05      18   0.15481E-03   0.97842E-02 0.10768E+02 
c  k            0.68447E-02      11   0.11843E-04   0.25879E-01 0.70066E+02 
c  omega        0.27922E+07       1   0.10116E-06   0.11215E+08 0.52998E+00 
c  TempK        0.96421E+04       7   0.29820E-05   0.90775E+02 0.33311E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.9343e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.154       0.0082235      -0.0085583
v  Velocity[Y]             -15.568          15.131        0.085477         0.12081
v  Velocity[Z]              -25.97          12.821         -1.6474        -0.50907
v  ǁVelocityǁ         0.00096684          26.145          7.7441          6.7229
v  Pressure                -545.98          212.75          35.442          38.918
v  k                   1.0165e-010          7.6951         0.11262         0.19137
v  omega                    57.512     2.7325e+008     1.2912e+006           76789
v  TempK                    298.17          363.17          329.06          332.39
v  TurbVisc            2.5472e-018      0.00046972       2.67e-005     8.3865e-005
v  CourantNb            0.00010345          1.4421         0.79771          0.9767
v  FourierNb             0.0036976               1         0.38821         0.10587
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046887      7.352e-005      0.00019578

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.57             306
v  Yplus               0          2.9603         0.63267           0.488


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64681          2.0244          1.1859          1.0826


 INSTANT    0.363000000E-02   TIME STEP NUMBER             363
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924349E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18385E-01 0.47046E+01
   Friction velocity        uk    :  0.18385E-01 0.47006E+01
   Dimensionless distance   yplus :  0.12465E-01 0.29604E+01
   Friction thermal sca.    tstar :  0.96837E-01 0.14525E+03
   Rough dim-less th. sca.  tplus :  0.88303E-02 0.20972E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27129E+00       9   0.39994E-05   0.16910E+01 0.21717E+02 
c  Velocity[X]                                      0.61164E+00 
c  Velocity[Y]                                      0.61436E+00 
c  Velocity[Z]                                      0.46496E+00 
c  Pressure     0.10341E-04      17   0.15268E-03   0.10252E-01 0.10580E+02 
c  k            0.68847E-02      11   0.11696E-04   0.25760E-01 0.69571E+02 
c  omega        0.27922E+07       1   0.10012E-06   0.11240E+08 0.53440E+00 
c  TempK        0.96465E+04       7   0.29653E-05   0.89429E+02 0.33136E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.9227e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.158       0.0082134      -0.0086099
v  Velocity[Y]             -15.566          15.142        0.085806         0.12126
v  Velocity[Z]             -25.973          12.848         -1.6479        -0.50929
v  ǁVelocityǁ         0.00096598          26.147           7.745          6.7242
v  Pressure                -545.71          212.81          35.492          38.957
v  k                   1.0166e-010          7.6818         0.11296         0.19245
v  omega                    57.513     2.7325e+008     1.2912e+006           76791
v  TempK                    298.18          363.17          329.11          332.46
v  TurbVisc            2.5473e-018      0.00047222     2.6797e-005      8.434e-005
v  CourantNb            0.00010386          1.4445         0.79773          0.9767
v  FourierNb             0.0036974               1         0.38827          0.1061
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0047505     7.3509e-005      0.00019576

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.58          306.01
v  Yplus               0          2.9604         0.63279         0.48818


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.36421          2.0268           1.186          1.0828


 INSTANT    0.364000000E-02   TIME STEP NUMBER             364
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924279E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18397E-01 0.47046E+01
   Friction velocity        uk    :  0.18397E-01 0.47006E+01
   Dimensionless distance   yplus :  0.12474E-01 0.29606E+01
   Friction thermal sca.    tstar :  0.10306E+00 0.14515E+03
   Rough dim-less th. sca.  tplus :  0.88365E-02 0.20973E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27140E+00       9   0.39767E-05   0.16680E+01 0.21538E+02 
c  Velocity[X]                                      0.60441E+00 
c  Velocity[Y]                                      0.60055E+00 
c  Velocity[Z]                                      0.46309E+00 
c  Pressure     0.10092E-04      17   0.15158E-03   0.10003E-01 0.10077E+02 
c  k            0.69248E-02      11   0.11547E-04   0.25643E-01 0.69093E+02 
c  omega        0.27922E+07       1   0.96777E-07   0.59195E+07 0.41308E+00 
c  TempK        0.96508E+04       7   0.29488E-05   0.88111E+02 0.32960E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.9109e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.162       0.0082033      -0.0086635
v  Velocity[Y]             -15.592          15.152        0.086136         0.12171
v  Velocity[Z]             -25.976          12.988         -1.6484        -0.50951
v  ǁVelocityǁ         0.00096517           26.15          7.7458          6.7254
v  Pressure                -545.43          212.86          35.538          38.992
v  k                   1.0167e-010          7.6683         0.11329         0.19352
v  omega                    57.513     2.7325e+008     1.2912e+006           76793
v  TempK                    298.18          363.17          329.15          332.52
v  TurbVisc            2.5475e-018      0.00047459     2.6895e-005     8.4814e-005
v  CourantNb            0.00010422           1.447         0.79775         0.97671
v  FourierNb             0.0036972               1         0.38833         0.10632
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0048162     7.3498e-005      0.00019574

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.58          306.01
v  Yplus               0          2.9606         0.63291         0.48835


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.34691          2.0294          1.1861           1.083


 INSTANT    0.365000000E-02   TIME STEP NUMBER             365
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924243E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18412E-01 0.47046E+01
   Friction velocity        uk    :  0.18412E-01 0.47005E+01
   Dimensionless distance   yplus :  0.12483E-01 0.29607E+01
   Friction thermal sca.    tstar :  0.10976E+00 0.14503E+03
   Rough dim-less th. sca.  tplus :  0.88433E-02 0.20974E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27151E+00       9   0.39496E-05   0.16265E+01 0.21387E+02 
c  Velocity[X]                                      0.59726E+00 
c  Velocity[Y]                                      0.58910E+00 
c  Velocity[Z]                                      0.44019E+00 
c  Pressure     0.98034E-05      17   0.15038E-03   0.97156E-02 0.10554E+02 
c  k            0.69650E-02      11   0.11476E-04   0.25537E-01 0.68637E+02 
c  omega        0.27922E+07       1   0.96613E-07   0.81596E+07 0.46839E+00 
c  TempK        0.96550E+04       7   0.29328E-05   0.86809E+02 0.32782E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.8988e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258          19.166       0.0081888      -0.0087182
v  Velocity[Y]             -15.696          15.163        0.086463         0.12216
v  Velocity[Z]             -25.979          13.039         -1.6489        -0.50972
v  ǁVelocityǁ          0.0009645          26.153          7.7467          6.7266
v  Pressure                -545.13          212.91          35.588          39.031
v  k                   1.0167e-010          7.6547         0.11363          0.1946
v  omega                    57.513     2.7325e+008     1.2912e+006           76795
v  TempK                    298.18          363.17          329.19          332.58
v  TurbVisc            2.5476e-018      0.00047684     2.6992e-005     8.5287e-005
v  CourantNb            0.00010462          1.4495         0.79776         0.97671
v  FourierNb             0.0036971               1         0.38839         0.10654
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0048655     7.3487e-005      0.00019571

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.59          306.01
v  Yplus               0          2.9607         0.63302         0.48851


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4503           2.032          1.1862          1.0833


 INSTANT    0.366000000E-02   TIME STEP NUMBER             366
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924238E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18423E-01 0.47045E+01
   Friction velocity        uk    :  0.18423E-01 0.47005E+01
   Dimensionless distance   yplus :  0.12491E-01 0.29609E+01
   Friction thermal sca.    tstar :  0.11700E+00 0.14495E+03
   Rough dim-less th. sca.  tplus :  0.88486E-02 0.20975E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27162E+00       9   0.39331E-05   0.16062E+01 0.21287E+02 
c  Velocity[X]                                      0.59285E+00 
c  Velocity[Y]                                      0.58080E+00 
c  Velocity[Z]                                      0.43255E+00 
c  Pressure     0.97128E-05      16   0.14880E-03   0.96241E-02 0.10368E+02 
c  k            0.70053E-02      11   0.11413E-04   0.25447E-01 0.68212E+02 
c  omega        0.27922E+07       1   0.99002E-07   0.19927E+08 0.69255E+00 
c  TempK        0.96592E+04       7   0.29173E-05   0.85529E+02 0.32603E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.8868e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258           19.17       0.0081724      -0.0087746
v  Velocity[Y]             -15.737          15.173        0.086788         0.12261
v  Velocity[Z]             -25.982          13.207         -1.6494        -0.50992
v  ǁVelocityǁ         0.00096375          26.156          7.7475          6.7278
v  Pressure                -544.83          212.96          35.638          39.069
v  k                   1.0168e-010          7.6408         0.11397         0.19567
v  omega                    57.514     2.7325e+008     1.2912e+006           76796
v  TempK                    298.18          363.17          329.24          332.65
v  TurbVisc            2.5477e-018      0.00047896     2.7089e-005     8.5759e-005
v  CourantNb              0.000105          1.4521         0.79778         0.97671
v  FourierNb             0.0036969               1         0.38845         0.10676
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0048792     7.3477e-005      0.00019569

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           304.6          306.01
v  Yplus               0          2.9609         0.63313         0.48867


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.34749          2.0346          1.1862          1.0835


 INSTANT    0.367000000E-02   TIME STEP NUMBER             367
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924177E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18438E-01 0.47045E+01
   Friction velocity        uk    :  0.18438E-01 0.47005E+01
   Dimensionless distance   yplus :  0.12501E-01 0.29610E+01
   Friction thermal sca.    tstar :  0.12483E+00 0.14483E+03
   Rough dim-less th. sca.  tplus :  0.88558E-02 0.20976E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27173E+00       9   0.39181E-05   0.15773E+01 0.21155E+02 
c  Velocity[X]                                      0.58678E+00 
c  Velocity[Y]                                      0.57282E+00 
c  Velocity[Z]                                      0.41766E+00 
c  Pressure     0.95273E-05      15   0.14884E-03   0.94389E-02 0.10108E+02 
c  k            0.70456E-02      11   0.11401E-04   0.25338E-01 0.67760E+02 
c  omega        0.27922E+07       1   0.95384E-07   0.11524E+08 0.54597E+00 
c  TempK        0.96634E+04       7   0.29020E-05   0.84277E+02 0.32422E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.8753e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258          19.174        0.008152      -0.0088318
v  Velocity[Y]             -15.648          15.184        0.087118         0.12306
v  Velocity[Z]             -25.985          13.277         -1.6499        -0.51012
v  ǁVelocityǁ         0.00096287          26.159          7.7483           6.729
v  Pressure                -544.52          213.01          35.685          39.106
v  k                   1.0168e-010          7.6266          0.1143         0.19675
v  omega                    57.514     2.7324e+008     1.2912e+006           76798
v  TempK                    298.18          363.17          329.28          332.71
v  TurbVisc            2.5479e-018      0.00048096     2.7186e-005     8.6231e-005
v  CourantNb             0.0001054          1.4545         0.79779         0.97672
v  FourierNb             0.0036967               1         0.38852         0.10698
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0048706     7.3467e-005      0.00019566

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           304.6          306.02
v  Yplus               0           2.961         0.63324         0.48883


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62118           2.037          1.1863          1.0837


 INSTANT    0.368000000E-02   TIME STEP NUMBER             368
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924128E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18460E-01 0.47045E+01
   Friction velocity        uk    :  0.18460E-01 0.47005E+01
   Dimensionless distance   yplus :  0.12516E-01 0.29612E+01
   Friction thermal sca.    tstar :  0.13326E+00 0.14465E+03
   Rough dim-less th. sca.  tplus :  0.88667E-02 0.20977E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27183E+00       9   0.39034E-05   0.15523E+01 0.20992E+02 
c  Velocity[X]                                      0.58057E+00 
c  Velocity[Y]                                      0.55991E+00 
c  Velocity[Z]                                      0.41180E+00 
c  Pressure     0.99251E-05      15   0.15135E-03   0.98311E-02 0.10313E+02 
c  k            0.70860E-02      11   0.11333E-04   0.25211E-01 0.67276E+02 
c  omega        0.27922E+07       1   0.94717E-07   0.11861E+08 0.54883E+00 
c  TempK        0.96675E+04       7   0.28872E-05   0.83047E+02 0.32239E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.8641e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.259          19.178       0.0081286       -0.008891
v  Velocity[Y]             -15.594          15.194        0.087452         0.12351
v  Velocity[Z]             -25.987          13.469         -1.6504         -0.5103
v  ǁVelocityǁ         0.00096201          26.161           7.749          6.7301
v  Pressure                -544.25          213.07          35.734          39.144
v  k                   1.0169e-010           7.612         0.11464         0.19782
v  omega                    57.514     2.7324e+008     1.2912e+006           76800
v  TempK                    298.19          363.17          329.33          332.77
v  TurbVisc             2.548e-018      0.00048285     2.7283e-005     8.6701e-005
v  CourantNb            0.00010575          1.4569          0.7978         0.97672
v  FourierNb             0.0036966               1         0.38858          0.1072
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0048484     7.3458e-005      0.00019564

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.61          306.02
v  Yplus               0          2.9612         0.63334         0.48898


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.36187          2.0395          1.1864          1.0839


 INSTANT    0.369000000E-02   TIME STEP NUMBER             369
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924078E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18484E-01 0.47044E+01
   Friction velocity        uk    :  0.18484E-01 0.47004E+01
   Dimensionless distance   yplus :  0.12532E-01 0.29612E+01
   Friction thermal sca.    tstar :  0.14241E+00 0.14446E+03
   Rough dim-less th. sca.  tplus :  0.88780E-02 0.20978E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27194E+00       9   0.38890E-05   0.15338E+01 0.20907E+02 
c  Velocity[X]                                      0.57645E+00 
c  Velocity[Y]                                      0.55296E+00 
c  Velocity[Z]                                      0.40437E+00 
c  Pressure     0.96124E-05      16   0.15013E-03   0.95202E-02 0.91508E+01 
c  k            0.71264E-02      11   0.11304E-04   0.25075E-01 0.66774E+02 
c  omega        0.27922E+07       1   0.92701E-07   0.10345E+08 0.52175E+00 
c  TempK        0.96716E+04       7   0.28727E-05   0.81842E+02 0.32055E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.8526e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.259          19.182       0.0081071       -0.008951
v  Velocity[Y]             -15.593          15.205        0.087788         0.12396
v  Velocity[Z]              -25.99          13.558         -1.6509        -0.51049
v  ǁVelocityǁ         0.00096131          26.164          7.7498          6.7312
v  Pressure                -543.98          213.11          35.772          39.171
v  k                   1.0169e-010           7.597         0.11497         0.19889
v  omega                    57.514     2.7324e+008     1.2912e+006           76801
v  TempK                    298.19          363.17          329.37          332.84
v  TurbVisc            2.5481e-018      0.00048464     2.7379e-005      8.717e-005
v  CourantNb            0.00010618          1.4593         0.79782         0.97672
v  FourierNb             0.0036964               1         0.38864         0.10741
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0047243     7.3447e-005      0.00019562

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.61          306.02
v  Yplus               0          2.9612         0.63343         0.48913


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.8362           2.042          1.1865          1.0841


 INSTANT    0.370000000E-02   TIME STEP NUMBER             370
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924115E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18503E-01 0.47044E+01
   Friction velocity        uk    :  0.18503E-01 0.47004E+01
   Dimensionless distance   yplus :  0.12545E-01 0.29614E+01
   Friction thermal sca.    tstar :  0.15227E+00 0.14431E+03
   Rough dim-less th. sca.  tplus :  0.88871E-02 0.20978E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27204E+00       9   0.38769E-05   0.15037E+01 0.20709E+02 
c  Velocity[X]                                      0.57045E+00 
c  Velocity[Y]                                      0.54085E+00 
c  Velocity[Z]                                      0.39243E+00 
c  Pressure     0.97219E-05      15   0.14996E-03   0.96267E-02 0.87031E+01 
c  k            0.71669E-02      11   0.11232E-04   0.24941E-01 0.66281E+02 
c  omega        0.27922E+07       1   0.91980E-07   0.11208E+08 0.54309E+00 
c  TempK        0.96756E+04       7   0.28583E-05   0.80657E+02 0.31870E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.841e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.26          19.185       0.0080833      -0.0090114
v  Velocity[Y]             -15.637          15.215        0.088124         0.12442
v  Velocity[Z]             -25.992           13.78         -1.6514        -0.51066
v  ǁVelocityǁ         0.00096064          26.166          7.7505          6.7323
v  Pressure                 -543.7          213.15          35.809          39.198
v  k                    1.017e-010          7.5816         0.11531         0.19996
v  omega                    57.514     2.7324e+008     1.2912e+006           76803
v  TempK                    298.19          363.17          329.41           332.9
v  TurbVisc            2.5482e-018      0.00048631     2.7475e-005     8.7638e-005
v  CourantNb            0.00010656          1.4618         0.79782         0.97672
v  FourierNb             0.0036962               1         0.38871         0.10763
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0047744     7.3437e-005       0.0001956

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.62          306.02
v  Yplus               0          2.9614         0.63353         0.48927


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38565          2.0445          1.1865          1.0843


 INSTANT    0.371000000E-02   TIME STEP NUMBER             371
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924082E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18523E-01 0.47044E+01
   Friction velocity        uk    :  0.18523E-01 0.47003E+01
   Dimensionless distance   yplus :  0.12559E-01 0.29615E+01
   Friction thermal sca.    tstar :  0.16288E+00 0.14416E+03
   Rough dim-less th. sca.  tplus :  0.88967E-02 0.20979E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27214E+00       9   0.38696E-05   0.14853E+01 0.20613E+02 
c  Velocity[X]                                      0.56709E+00 
c  Velocity[Y]                                      0.53179E+00 
c  Velocity[Z]                                      0.38641E+00 
c  Pressure     0.96585E-05      16   0.15036E-03   0.95628E-02 0.92554E+01 
c  k            0.72075E-02      11   0.11187E-04   0.24814E-01 0.65786E+02 
c  omega        0.27922E+07       1   0.91429E-07   0.11730E+08 0.55040E+00 
c  TempK        0.96796E+04       7   0.28443E-05   0.79495E+02 0.31683E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.8291e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.26          19.189       0.0080597      -0.0090745
v  Velocity[Y]              -15.79          15.225        0.088457         0.12487
v  Velocity[Z]             -25.995          13.888         -1.6518        -0.51083
v  ǁVelocityǁ         0.00096021          26.169          7.7512          6.7334
v  Pressure                -543.42          213.19          35.848          39.227
v  k                    1.017e-010          7.5657         0.11564         0.20102
v  omega                    57.515     2.7324e+008     1.2912e+006           76805
v  TempK                     298.2          363.17          329.46          332.96
v  TurbVisc            2.5484e-018      0.00048788     2.7571e-005     8.8105e-005
v  CourantNb            0.00010695          1.4643         0.79783         0.97672
v  FourierNb             0.0036961               1         0.38877         0.10784
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0048082     7.3427e-005      0.00019557

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.62          306.03
v  Yplus               0          2.9615         0.63362         0.48941


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85038          2.0472          1.1866          1.0846


 INSTANT    0.372000000E-02   TIME STEP NUMBER             372
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924169E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18533E-01 0.47043E+01
   Friction velocity        uk    :  0.18533E-01 0.47003E+01
   Dimensionless distance   yplus :  0.12566E-01 0.29616E+01
   Friction thermal sca.    tstar :  0.17427E+00 0.14408E+03
   Rough dim-less th. sca.  tplus :  0.89016E-02 0.20980E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27223E+00       9   0.38657E-05   0.14707E+01 0.20542E+02 
c  Velocity[X]                                      0.56249E+00 
c  Velocity[Y]                                      0.52762E+00 
c  Velocity[Z]                                      0.38056E+00 
c  Pressure     0.97882E-05      15   0.15131E-03   0.96893E-02 0.84315E+01 
c  k            0.72481E-02      11   0.11121E-04   0.24684E-01 0.65288E+02 
c  omega        0.27922E+07       1   0.90048E-07   0.11757E+08 0.55749E+00 
c  TempK        0.96836E+04       7   0.28307E-05   0.78354E+02 0.31495E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.8179e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.261          19.193       0.0080345      -0.0091377
v  Velocity[Y]             -15.714          15.236        0.088792         0.12532
v  Velocity[Z]             -25.998          14.144         -1.6523        -0.51099
v  ǁVelocityǁ         0.00095944          26.172          7.7519          6.7345
v  Pressure                -543.14          213.23          35.882          39.251
v  k                    1.017e-010          7.5493         0.11598         0.20209
v  omega                    57.515     2.7324e+008     1.2912e+006           76806
v  TempK                     298.2          363.17           329.5          333.02
v  TurbVisc            2.5485e-018      0.00048935     2.7667e-005     8.8571e-005
v  CourantNb            0.00010732          1.4667         0.79784         0.97672
v  FourierNb             0.0036959               1         0.38884         0.10806
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0048456     7.3417e-005      0.00019555

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.63          306.03
v  Yplus               0          2.9616         0.63371         0.48954


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43215          2.0496          1.1867          1.0848


 INSTANT    0.373000000E-02   TIME STEP NUMBER             373
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923993E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18561E-01 0.47043E+01
   Friction velocity        uk    :  0.18561E-01 0.47002E+01
   Dimensionless distance   yplus :  0.12584E-01 0.29618E+01
   Friction thermal sca.    tstar :  0.18276E+00 0.14386E+03
   Rough dim-less th. sca.  tplus :  0.89149E-02 0.20981E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27233E+00       9   0.38538E-05   0.14421E+01 0.20340E+02 
c  Velocity[X]                                      0.55607E+00 
c  Velocity[Y]                                      0.51472E+00 
c  Velocity[Z]                                      0.37131E+00 
c  Pressure     0.92697E-05      14   0.14393E-03   0.91751E-02 0.84450E+01 
c  k            0.72888E-02      11   0.11037E-04   0.24553E-01 0.64786E+02 
c  omega        0.27922E+07       1   0.87958E-07   0.92964E+07 0.50703E+00 
c  TempK        0.96875E+04       7   0.28168E-05   0.77235E+02 0.31307E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.8071e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.261          19.196       0.0080098      -0.0092027
v  Velocity[Y]             -15.637          15.246        0.089128         0.12577
v  Velocity[Z]             -26.001          14.271         -1.6527        -0.51114
v  ǁVelocityǁ         0.00095865          26.175          7.7526          6.7356
v  Pressure                -542.87          213.26          35.915          39.274
v  k                   1.0171e-010          7.5325         0.11631         0.20315
v  omega                    57.515     2.7324e+008     1.2912e+006           76808
v  TempK                     298.2          363.17          329.54          333.08
v  TurbVisc            2.5486e-018      0.00049073     2.7763e-005     8.9036e-005
v  CourantNb            0.00010772           1.469         0.79785         0.97672
v  FourierNb             0.0036957               1         0.38891         0.10827
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0048864     7.3408e-005      0.00019553

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.64          306.03
v  Yplus               0          2.9618         0.63379         0.48967


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67398           2.052          1.1868           1.085


 INSTANT    0.374000000E-02   TIME STEP NUMBER             374
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923976E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18591E-01 0.47042E+01
   Friction velocity        uk    :  0.18591E-01 0.47002E+01
   Dimensionless distance   yplus :  0.12605E-01 0.29619E+01
   Friction thermal sca.    tstar :  0.18896E+00 0.14362E+03
   Rough dim-less th. sca.  tplus :  0.89295E-02 0.20982E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27242E+00       9   0.38543E-05   0.14281E+01 0.20221E+02 
c  Velocity[X]                                      0.55223E+00 
c  Velocity[Y]                                      0.50588E+00 
c  Velocity[Z]                                      0.36994E+00 
c  Pressure     0.10013E-04      15   0.14775E-03   0.99087E-02 0.85583E+01 
c  k            0.73295E-02      11   0.11037E-04   0.24428E-01 0.64305E+02 
c  omega        0.27922E+07       1   0.85981E-07   0.69643E+07 0.45226E+00 
c  TempK        0.96914E+04       7   0.28030E-05   0.76136E+02 0.31116E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7961e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.261          19.199       0.0079813      -0.0092692
v  Velocity[Y]             -15.611          15.256        0.089464         0.12622
v  Velocity[Z]             -26.004          14.561         -1.6531        -0.51129
v  ǁVelocityǁ         0.00095801          26.178          7.7533          6.7366
v  Pressure                -542.58           213.3          35.951          39.301
v  k                   1.0171e-010          7.5151         0.11665         0.20421
v  omega                    57.515     2.7323e+008     1.2912e+006           76809
v  TempK                    298.21          363.17          329.58          333.14
v  TurbVisc            2.5487e-018      0.00049203     2.7858e-005     8.9499e-005
v  CourantNb            0.00010811          1.4714         0.79785         0.97672
v  FourierNb             0.0036956               1         0.38897         0.10848
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0049218     7.3399e-005       0.0001955

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.64          306.03
v  Yplus               0          2.9619         0.63388          0.4898


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.31764          2.0545          1.1868          1.0852


 INSTANT    0.375000000E-02   TIME STEP NUMBER             375
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924022E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18616E-01 0.47041E+01
   Friction velocity        uk    :  0.18616E-01 0.47001E+01
   Dimensionless distance   yplus :  0.12622E-01 0.29621E+01
   Friction thermal sca.    tstar :  0.19512E+00 0.14343E+03
   Rough dim-less th. sca.  tplus :  0.89416E-02 0.20983E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27251E+00       9   0.38545E-05   0.14241E+01 0.20180E+02 
c  Velocity[X]                                      0.55038E+00 
c  Velocity[Y]                                      0.49920E+00 
c  Velocity[Z]                                      0.37449E+00 
c  Pressure     0.94260E-05      15   0.14771E-03   0.93277E-02 0.88524E+01 
c  k            0.73702E-02      11   0.11005E-04   0.24342E-01 0.63915E+02 
c  omega        0.27922E+07       1   0.86768E-07   0.10637E+08 0.53343E+00 
c  TempK        0.96953E+04       7   0.27892E-05   0.75050E+02 0.30924E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7848e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.262          19.203       0.0079549      -0.0093372
v  Velocity[Y]             -15.633          15.266        0.089807         0.12668
v  Velocity[Z]             -26.007          14.702         -1.6536        -0.51142
v  ǁVelocityǁ         0.00095746           26.18          7.7539          6.7376
v  Pressure                 -542.3          213.34          35.986          39.326
v  k                   1.0172e-010          7.4973         0.11698         0.20526
v  omega                    57.516     2.7323e+008     1.2912e+006           76811
v  TempK                    298.21          363.17          329.63           333.2
v  TurbVisc            2.5488e-018      0.00049326     2.7953e-005     8.9961e-005
v  CourantNb             0.0001085          1.4739         0.79786         0.97672
v  FourierNb             0.0036954               1         0.38904         0.10869
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0049419      7.339e-005      0.00019548

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.65          306.04
v  Yplus               0          2.9621         0.63395         0.48992


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44401           2.057          1.1869          1.0854


 INSTANT    0.376000000E-02   TIME STEP NUMBER             376
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924068E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18638E-01 0.47041E+01
   Friction velocity        uk    :  0.18638E-01 0.47001E+01
   Dimensionless distance   yplus :  0.12637E-01 0.29621E+01
   Friction thermal sca.    tstar :  0.20164E+00 0.14326E+03
   Rough dim-less th. sca.  tplus :  0.89522E-02 0.20984E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27260E+00       9   0.38523E-05   0.13988E+01 0.20121E+02 
c  Velocity[X]                                      0.54813E+00 
c  Velocity[Y]                                      0.49472E+00 
c  Velocity[Z]                                      0.35597E+00 
c  Pressure     0.92796E-05      14   0.14632E-03   0.91820E-02 0.82584E+01 
c  k            0.74109E-02      11   0.10982E-04   0.24286E-01 0.63597E+02 
c  omega        0.27922E+07       1   0.87317E-07   0.14347E+08 0.60514E+00 
c  TempK        0.96991E+04       7   0.27752E-05   0.73983E+02 0.30730E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7731e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.262          19.206       0.0079275      -0.0094055
v  Velocity[Y]             -15.736          15.276        0.090146         0.12713
v  Velocity[Z]             -26.009          15.025          -1.654        -0.51156
v  ǁVelocityǁ         0.00095699          26.183          7.7545          6.7386
v  Pressure                   -542          213.38           36.02          39.349
v  k                   1.0172e-010           7.479         0.11731         0.20632
v  omega                    57.516     2.7323e+008     1.2912e+006           76812
v  TempK                    298.21          363.17          329.67          333.26
v  TurbVisc            2.5489e-018      0.00049575     2.8048e-005     9.0422e-005
v  CourantNb            0.00010893          1.4764         0.79786         0.97672
v  FourierNb             0.0036952               1          0.3891          0.1089
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0049563     7.3382e-005      0.00019546

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.65          306.04
v  Yplus               0          2.9621         0.63403         0.49003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4857          2.0596           1.187          1.0856


 INSTANT    0.377000000E-02   TIME STEP NUMBER             377
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924051E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18657E-01 0.47040E+01
   Friction velocity        uk    :  0.18657E-01 0.47000E+01
   Dimensionless distance   yplus :  0.12650E-01 0.29623E+01
   Friction thermal sca.    tstar :  0.20856E+00 0.14311E+03
   Rough dim-less th. sca.  tplus :  0.89613E-02 0.20985E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27269E+00       9   0.38501E-05   0.13851E+01 0.19995E+02 
c  Velocity[X]                                      0.54557E+00 
c  Velocity[Y]                                      0.48602E+00 
c  Velocity[Z]                                      0.35351E+00 
c  Pressure     0.90523E-05      15   0.14177E-03   0.89564E-02 0.76180E+01 
c  k            0.74517E-02      11   0.10930E-04   0.24179E-01 0.63174E+02 
c  omega        0.27922E+07       1   0.88628E-07   0.21410E+08 0.72453E+00 
c  TempK        0.97029E+04       7   0.27611E-05   0.72932E+02 0.30535E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7616e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.262          19.209       0.0079003      -0.0094757
v  Velocity[Y]              -15.78          15.286        0.090485         0.12759
v  Velocity[Z]             -26.012           15.17         -1.6544        -0.51168
v  ǁVelocityǁ         0.00095653          26.185          7.7551          6.7396
v  Pressure                -541.71          213.41          36.045          39.365
v  k                   1.0172e-010          7.4602         0.11765         0.20737
v  omega                    57.516     2.7323e+008     1.2912e+006           76814
v  TempK                    298.22          363.17          329.71          333.33
v  TurbVisc             2.549e-018      0.00049852     2.8143e-005     9.0881e-005
v  CourantNb             0.0001093          1.4789         0.79786         0.97672
v  FourierNb              0.003695               1         0.38917         0.10911
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.004957     7.3374e-005      0.00019544

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.66          306.04
v  Yplus               0          2.9623          0.6341         0.49014


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35745          2.0622           1.187          1.0858


 INSTANT    0.378000000E-02   TIME STEP NUMBER             378
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923969E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18678E-01 0.47039E+01
   Friction velocity        uk    :  0.18678E-01 0.46999E+01
   Dimensionless distance   yplus :  0.12664E-01 0.29624E+01
   Friction thermal sca.    tstar :  0.21595E+00 0.14295E+03
   Rough dim-less th. sca.  tplus :  0.89711E-02 0.20986E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27278E+00       9   0.38484E-05   0.13686E+01 0.19895E+02 
c  Velocity[X]                                      0.54317E+00 
c  Velocity[Y]                                      0.48012E+00 
c  Velocity[Z]                                      0.34529E+00 
c  Pressure     0.90195E-05      14   0.14137E-03   0.89230E-02 0.77527E+01 
c  k            0.74925E-02      11   0.10985E-04   0.24065E-01 0.62728E+02 
c  omega        0.27922E+07       1   0.82503E-07   0.87265E+07 0.49856E+00 
c  TempK        0.97066E+04       7   0.27470E-05   0.71900E+02 0.30339E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7507e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.263          19.211       0.0078694      -0.0095472
v  Velocity[Y]             -15.695          15.295        0.090825         0.12804
v  Velocity[Z]             -26.015           15.52         -1.6547         -0.5118
v  ǁVelocityǁ         0.00095588          26.188          7.7557          6.7406
v  Pressure                -541.41          213.44          36.073          39.384
v  k                   1.0173e-010          7.4412         0.11798         0.20842
v  omega                    57.516     2.7323e+008     1.2912e+006           76815
v  TempK                    298.22          363.17          329.75          333.38
v  TurbVisc            2.5491e-018      0.00050128     2.8237e-005     9.1338e-005
v  CourantNb            0.00010972          1.4813         0.79787         0.97672
v  FourierNb             0.0036948               1         0.38924         0.10932
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0049366     7.3366e-005      0.00019542

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.66          306.04
v  Yplus               0          2.9624         0.63416         0.49025


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.80178          2.0646          1.1871           1.086


 INSTANT    0.379000000E-02   TIME STEP NUMBER             379
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924032E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18709E-01 0.47038E+01
   Friction velocity        uk    :  0.18709E-01 0.46998E+01
   Dimensionless distance   yplus :  0.12685E-01 0.29625E+01
   Friction thermal sca.    tstar :  0.22331E+00 0.14271E+03
   Rough dim-less th. sca.  tplus :  0.89862E-02 0.20987E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27286E+00       9   0.38482E-05   0.13536E+01 0.19738E+02 
c  Velocity[X]                                      0.54139E+00 
c  Velocity[Y]                                      0.46866E+00 
c  Velocity[Z]                                      0.34359E+00 
c  Pressure     0.90937E-05      15   0.14246E-03   0.89959E-02 0.73638E+01 
c  k            0.75333E-02      11   0.10926E-04   0.23943E-01 0.62265E+02 
c  omega        0.27922E+07       1   0.79560E-07   0.44460E+07 0.39301E+00 
c  TempK        0.97103E+04       7   0.27328E-05   0.70885E+02 0.30143E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step       6.74e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.263          19.214       0.0078377      -0.0096206
v  Velocity[Y]             -15.638          15.305        0.091164          0.1285
v  Velocity[Z]             -26.018          15.661         -1.6551        -0.51191
v  ǁVelocityǁ         0.00095526          26.191          7.7563          6.7415
v  Pressure                -541.12          213.46          36.096          39.399
v  k                   1.0173e-010          7.4218         0.11831         0.20946
v  omega                    57.516     2.7323e+008     1.2912e+006           76817
v  TempK                    298.23          363.17           329.8          333.44
v  TurbVisc            2.5492e-018      0.00050403     2.8331e-005     9.1794e-005
v  CourantNb            0.00011012          1.4837         0.79787         0.97672
v  FourierNb             0.0036948               1         0.38931         0.10952
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0049097     7.3359e-005      0.00019541

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.67          306.05
v  Yplus               0          2.9625         0.63423         0.49035


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.32338           2.067          1.1872          1.0862


 INSTANT    0.380000000E-02   TIME STEP NUMBER             380
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924082E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18740E-01 0.47038E+01
   Friction velocity        uk    :  0.18740E-01 0.46997E+01
   Dimensionless distance   yplus :  0.12706E-01 0.29627E+01
   Friction thermal sca.    tstar :  0.22927E+00 0.14247E+03
   Rough dim-less th. sca.  tplus :  0.90011E-02 0.20988E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27294E+00       9   0.38543E-05   0.13444E+01 0.19650E+02 
c  Velocity[X]                                      0.54012E+00 
c  Velocity[Y]                                      0.46164E+00 
c  Velocity[Z]                                      0.34259E+00 
c  Pressure     0.92240E-05      14   0.14587E-03   0.91242E-02 0.74943E+01 
c  k            0.75741E-02      11   0.10917E-04   0.23821E-01 0.61814E+02 
c  omega        0.27922E+07       1   0.78364E-07   0.39715E+07 0.38091E+00 
c  TempK        0.97140E+04       7   0.27183E-05   0.69888E+02 0.29946E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7292e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.263          19.217       0.0078063      -0.0096948
v  Velocity[Y]             -15.628          15.315        0.091505         0.12895
v  Velocity[Z]             -26.021          16.041         -1.6555        -0.51202
v  ǁVelocityǁ         0.00095477          26.194          7.7569          6.7425
v  Pressure                -540.83          213.49          36.123          39.416
v  k                   1.0174e-010          7.4023         0.11864          0.2105
v  omega                    57.516     2.7322e+008     1.2912e+006           76818
v  TempK                    298.23          363.17          329.84           333.5
v  TurbVisc            2.5493e-018      0.00050677     2.8425e-005     9.2249e-005
v  CourantNb            0.00011055          1.4861         0.79787         0.97672
v  FourierNb             0.0036948               1         0.38938         0.10973
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0048828     7.3352e-005      0.00019539

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.67          306.05
v  Yplus               0          2.9627         0.63429         0.49045


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83917          2.0695          1.1872          1.0865


 INSTANT    0.381000000E-02   TIME STEP NUMBER             381
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924023E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18766E-01 0.47037E+01
   Friction velocity        uk    :  0.18766E-01 0.46996E+01
   Dimensionless distance   yplus :  0.12724E-01 0.29628E+01
   Friction thermal sca.    tstar :  0.23555E+00 0.14228E+03
   Rough dim-less th. sca.  tplus :  0.90135E-02 0.20989E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27303E+00       9   0.38555E-05   0.13295E+01 0.19569E+02 
c  Velocity[X]                                      0.53923E+00 
c  Velocity[Y]                                      0.45515E+00 
c  Velocity[Z]                                      0.33517E+00 
c  Pressure     0.89008E-05      15   0.14270E-03   0.88043E-02 0.73401E+01 
c  k            0.76149E-02      11   0.10920E-04   0.23709E-01 0.61386E+02 
c  omega        0.27922E+07       1   0.78445E-07   0.59080E+07 0.43341E+00 
c  TempK        0.97176E+04       7   0.27036E-05   0.68908E+02 0.29749E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7182e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.264           19.22       0.0077743      -0.0097702
v  Velocity[Y]             -15.648          15.325        0.091848          0.1294
v  Velocity[Z]             -26.024          16.169         -1.6558        -0.51212
v  ǁVelocityǁ         0.00095433          26.196          7.7574          6.7434
v  Pressure                -540.54          213.52          36.148          39.432
v  k                   1.0174e-010          7.3827         0.11897         0.21154
v  omega                    57.517     2.7322e+008     1.2912e+006           76820
v  TempK                    298.23          363.17          329.88          333.56
v  TurbVisc            2.5493e-018      0.00050949     2.8519e-005     9.2702e-005
v  CourantNb            0.00011093          1.4885         0.79787         0.97672
v  FourierNb              0.003695               1         0.38944         0.10994
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.004862     7.3345e-005      0.00019537

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.68          306.05
v  Yplus               0          2.9628         0.63435         0.49055


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40999           2.072          1.1873          1.0867


 INSTANT    0.382000000E-02   TIME STEP NUMBER             382
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923979E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18790E-01 0.47036E+01
   Friction velocity        uk    :  0.18790E-01 0.46996E+01
   Dimensionless distance   yplus :  0.12740E-01 0.29630E+01
   Friction thermal sca.    tstar :  0.24229E+00 0.14209E+03
   Rough dim-less th. sca.  tplus :  0.90251E-02 0.20990E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27311E+00       9   0.38585E-05   0.13249E+01 0.19573E+02 
c  Velocity[X]                                      0.53892E+00 
c  Velocity[Y]                                      0.45207E+00 
c  Velocity[Z]                                      0.33391E+00 
c  Pressure     0.91254E-05      15   0.14227E-03   0.90259E-02 0.79597E+01 
c  k            0.76557E-02      11   0.10854E-04   0.23600E-01 0.60973E+02 
c  omega        0.27922E+07       1   0.80894E-07   0.12184E+08 0.56444E+00 
c  TempK        0.97212E+04       6   0.51543E-05   0.66638E+02 0.29263E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7069e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.264          19.222       0.0077426      -0.0098457
v  Velocity[Y]             -15.749          15.334        0.092193         0.12986
v  Velocity[Z]             -26.026          16.582         -1.6562        -0.51221
v  ǁVelocityǁ         0.00095398          26.199           7.758          6.7443
v  Pressure                -540.24          213.55          36.179          39.453
v  k                   1.0174e-010          7.3631          0.1193         0.21258
v  omega                    57.517     2.7322e+008     1.2912e+006           76821
v  TempK                    298.23          363.17          329.92          333.62
v  TurbVisc            2.5494e-018      0.00051219     2.8612e-005     9.3153e-005
v  CourantNb            0.00011136           1.491         0.79787         0.97672
v  FourierNb             0.0036951               1         0.38951         0.11014
v  total_pressure      1.0078e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0048384     7.3338e-005      0.00019536

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.68          306.05
v  Yplus               0           2.963         0.63441         0.49064


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.84463          2.0745          1.1874          1.0869


 INSTANT    0.383000000E-02   TIME STEP NUMBER             383
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923984E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18810E-01 0.47035E+01
   Friction velocity        uk    :  0.18810E-01 0.46995E+01
   Dimensionless distance   yplus :  0.12753E-01 0.29630E+01
   Friction thermal sca.    tstar :  0.24928E+00 0.14194E+03
   Rough dim-less th. sca.  tplus :  0.90344E-02 0.20990E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27319E+00       9   0.38657E-05   0.13257E+01 0.19567E+02 
c  Velocity[X]                                      0.54064E+00 
c  Velocity[Y]                                      0.44897E+00 
c  Velocity[Z]                                      0.33610E+00 
c  Pressure     0.94499E-05      14   0.14022E-03   0.93465E-02 0.70921E+01 
c  k            0.76965E-02      11   0.10859E-04   0.23496E-01 0.60579E+02 
c  omega        0.27922E+07       1   0.82976E-07   0.22058E+08 0.73157E+00 
c  TempK        0.97248E+04       6   0.51272E-05   0.65726E+02 0.29072E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6959e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.264          19.225       0.0077134      -0.0099216
v  Velocity[Y]             -15.789          15.343        0.092538         0.13032
v  Velocity[Z]             -26.028          16.687         -1.6566         -0.5123
v  ǁVelocityǁ         0.00053215          26.201          7.7585          6.7452
v  Pressure                -539.95          213.58            36.2          39.465
v  k                   1.0174e-010          7.3436         0.11963         0.21361
v  omega                    57.517     2.7322e+008     1.2912e+006           76822
v  TempK                    298.23          363.17          329.96          333.68
v  TurbVisc            2.5495e-018      0.00051488     2.8705e-005     9.3602e-005
v  CourantNb             0.0001118          1.4935         0.79787         0.97672
v  FourierNb             0.0036952               1         0.38958         0.11034
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0051389     7.3331e-005      0.00019534

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.69          306.05
v  Yplus               0           2.963         0.63446         0.49073


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.30876          2.0771          1.1874          1.0871


 INSTANT    0.384000000E-02   TIME STEP NUMBER             384
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924069E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18833E-01 0.47034E+01
   Friction velocity        uk    :  0.18833E-01 0.46994E+01
   Dimensionless distance   yplus :  0.12769E-01 0.29631E+01
   Friction thermal sca.    tstar :  0.25680E+00 0.14177E+03
   Rough dim-less th. sca.  tplus :  0.90455E-02 0.20991E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27326E+00       9   0.38762E-05   0.13212E+01 0.19488E+02 
c  Velocity[X]                                      0.54023E+00 
c  Velocity[Y]                                      0.44448E+00 
c  Velocity[Z]                                      0.33649E+00 
c  Pressure     0.95369E-05      14   0.14283E-03   0.94320E-02 0.66573E+01 
c  k            0.77372E-02      11   0.10861E-04   0.23393E-01 0.60195E+02 
c  omega        0.27922E+07       1   0.77986E-07   0.11815E+08 0.55946E+00 
c  TempK        0.97283E+04       6   0.50995E-05   0.64830E+02 0.28882E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6854e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.265          19.227       0.0076826      -0.0099981
v  Velocity[Y]             -15.701          15.353        0.092884         0.13077
v  Velocity[Z]             -26.031          17.137         -1.6569        -0.51238
v  ǁVelocityǁ         0.00095308          26.203           7.759          6.7461
v  Pressure                -539.68          213.59          36.213           39.47
v  k                   1.0175e-010          7.3243         0.11996         0.21464
v  omega                    57.517     2.7322e+008     1.2912e+006           76824
v  TempK                    298.23          363.17             330          333.74
v  TurbVisc            2.5496e-018      0.00051754     2.8798e-005      9.405e-005
v  CourantNb            0.00011221          1.4958         0.79786         0.97672
v  FourierNb              0.003695               1         0.38965         0.11054
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0052816     7.3325e-005      0.00019532

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.69          306.06
v  Yplus               0          2.9631         0.63451         0.49081


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87569          2.0795          1.1875          1.0873


 INSTANT    0.385000000E-02   TIME STEP NUMBER             385
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924059E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18864E-01 0.47033E+01
   Friction velocity        uk    :  0.18864E-01 0.46992E+01
   Dimensionless distance   yplus :  0.12790E-01 0.29632E+01
   Friction thermal sca.    tstar :  0.26456E+00 0.14153E+03
   Rough dim-less th. sca.  tplus :  0.90606E-02 0.20992E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27334E+00       9   0.38818E-05   0.12995E+01 0.19312E+02 
c  Velocity[X]                                      0.54047E+00 
c  Velocity[Y]                                      0.43298E+00 
c  Velocity[Z]                                      0.32607E+00 
c  Pressure     0.91728E-05      14   0.13921E-03   0.90718E-02 0.66375E+01 
c  k            0.77780E-02      11   0.10792E-04   0.23296E-01 0.59823E+02 
c  omega        0.27922E+07       1   0.73643E-07   0.41502E+07 0.37431E+00 
c  TempK        0.97319E+04       6   0.50713E-05   0.63948E+02 0.28692E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6751e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.265           19.23       0.0076513       -0.010075
v  Velocity[Y]             -15.649          15.362         0.09323         0.13123
v  Velocity[Z]             -26.033          17.206         -1.6572        -0.51245
v  ǁVelocityǁ         0.00095259          26.206          7.7595          6.7469
v  Pressure                -539.38          213.61          36.229          39.478
v  k                   1.0175e-010          7.3052         0.12029         0.21566
v  omega                    57.517     2.7322e+008     1.2912e+006           76825
v  TempK                    298.23          363.17          330.04          333.79
v  TurbVisc            2.5496e-018      0.00052019      2.889e-005     9.4495e-005
v  CourantNb            0.00011267          1.4981         0.79786         0.97672
v  FourierNb             0.0036947               1         0.38972         0.11074
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0053454     7.3318e-005      0.00019531

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           304.7          306.06
v  Yplus               0          2.9632         0.63455          0.4909


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5167          2.0818          1.1876          1.0875


 INSTANT    0.386000000E-02   TIME STEP NUMBER             386
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924175E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18895E-01 0.47031E+01
   Friction velocity        uk    :  0.18895E-01 0.46991E+01
   Dimensionless distance   yplus :  0.12811E-01 0.29634E+01
   Friction thermal sca.    tstar :  0.27159E+00 0.14130E+03
   Rough dim-less th. sca.  tplus :  0.90754E-02 0.20993E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27342E+00       9   0.38903E-05   0.12905E+01 0.19242E+02 
c  Velocity[X]                                      0.53968E+00 
c  Velocity[Y]                                      0.42687E+00 
c  Velocity[Z]                                      0.32395E+00 
c  Pressure     0.92617E-05      14   0.14164E-03   0.91594E-02 0.64807E+01 
c  k            0.78187E-02      11   0.10794E-04   0.23203E-01 0.59462E+02 
c  omega        0.27922E+07       1   0.72354E-07   0.33994E+07 0.35342E+00 
c  TempK        0.97353E+04       6   0.50425E-05   0.63082E+02 0.28504E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6646e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.265          19.232        0.007619       -0.010153
v  Velocity[Y]              -15.65          15.371        0.093576         0.13168
v  Velocity[Z]             -26.036          17.702         -1.6575        -0.51252
v  ǁVelocityǁ         0.00095224          26.208            7.76          6.7478
v  Pressure                -539.08          213.63          36.245          39.485
v  k                   1.0175e-010          7.2865         0.12061         0.21668
v  omega                    57.517     2.7321e+008     1.2912e+006           76826
v  TempK                    298.23          363.17          330.08          333.85
v  TurbVisc            2.5497e-018      0.00052283     2.8982e-005     9.4939e-005
v  CourantNb            0.00011308          1.5005         0.79786         0.97672
v  FourierNb             0.0036944               1         0.38978         0.11094
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0053672     7.3312e-005      0.00019529

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           304.7          306.06
v  Yplus               0          2.9634          0.6346         0.49098


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73567          2.0842          1.1876          1.0877


 INSTANT    0.387000000E-02   TIME STEP NUMBER             387
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924223E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18919E-01 0.47030E+01
   Friction velocity        uk    :  0.18918E-01 0.46990E+01
   Dimensionless distance   yplus :  0.12827E-01 0.29635E+01
   Friction thermal sca.    tstar :  0.27909E+00 0.14112E+03
   Rough dim-less th. sca.  tplus :  0.90868E-02 0.20994E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27349E+00       9   0.38978E-05   0.12853E+01 0.19189E+02 
c  Velocity[X]                                      0.54042E+00 
c  Velocity[Y]                                      0.42105E+00 
c  Velocity[Z]                                      0.32383E+00 
c  Pressure     0.89983E-05      14   0.13931E-03   0.88990E-02 0.63666E+01 
c  k            0.78594E-02      11   0.10715E-04   0.23101E-01 0.59101E+02 
c  omega        0.27922E+07       1   0.72366E-07   0.49184E+07 0.39673E+00 
c  TempK        0.97388E+04       6   0.50134E-05   0.62231E+02 0.28317E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.654e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.266          19.234       0.0075877       -0.010232
v  Velocity[Y]             -15.697           15.38        0.093923         0.13214
v  Velocity[Z]             -26.039          17.712         -1.6578        -0.51258
v  ǁVelocityǁ         0.00095194          26.211          7.7605          6.7486
v  Pressure                -538.76          213.65          36.258           39.49
v  k                   1.0175e-010          7.2681         0.12094         0.21769
v  omega                    57.517     2.7321e+008     1.2912e+006           76828
v  TempK                    298.24          363.17          330.12          333.91
v  TurbVisc            2.5498e-018      0.00052544     2.9074e-005      9.538e-005
v  CourantNb            0.00011354          1.5028         0.79785         0.97672
v  FourierNb             0.0036943               1         0.38985         0.11114
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0053744     7.3305e-005      0.00019528

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.71          306.06
v  Yplus               0          2.9635         0.63465         0.49106


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54869          2.0867          1.1877          1.0879


 INSTANT    0.388000000E-02   TIME STEP NUMBER             388
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924155E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18940E-01 0.47029E+01
   Friction velocity        uk    :  0.18940E-01 0.46989E+01
   Dimensionless distance   yplus :  0.12841E-01 0.29636E+01
   Friction thermal sca.    tstar :  0.28705E+00 0.14097E+03
   Rough dim-less th. sca.  tplus :  0.90969E-02 0.20994E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27356E+00       9   0.39029E-05   0.12828E+01 0.19182E+02 
c  Velocity[X]                                      0.54004E+00 
c  Velocity[Y]                                      0.41662E+00 
c  Velocity[Z]                                      0.32612E+00 
c  Pressure     0.92587E-05      14   0.14193E-03   0.91560E-02 0.69491E+01 
c  k            0.79000E-02      11   0.10691E-04   0.22990E-01 0.58732E+02 
c  omega        0.27922E+07       1   0.74624E-07   0.99822E+07 0.51480E+00 
c  TempK        0.97422E+04       6   0.49838E-05   0.61396E+02 0.28132E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6433e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.266          19.237       0.0075559       -0.010311
v  Velocity[Y]             -15.853          15.389        0.094266         0.13259
v  Velocity[Z]             -26.041          18.268         -1.6582        -0.51264
v  ǁVelocityǁ         0.00095182          26.213          7.7609          6.7494
v  Pressure                -538.42          213.67          36.277          39.501
v  k                   1.0176e-010          7.2502         0.12126         0.21871
v  omega                    57.518     2.7321e+008     1.2912e+006           76829
v  TempK                    298.24          363.17          330.16          333.97
v  TurbVisc            2.5498e-018      0.00052805     2.9165e-005      9.582e-005
v  CourantNb            0.00011396          1.5053         0.79785         0.97672
v  FourierNb             0.0036943               1         0.38992         0.11134
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0053786       7.33e-005      0.00019526

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.71          306.06
v  Yplus               0          2.9636         0.63469         0.49113


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.84517          2.0892          1.1878          1.0881


 INSTANT    0.389000000E-02   TIME STEP NUMBER             389
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924113E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18949E-01 0.47028E+01
   Friction velocity        uk    :  0.18949E-01 0.46988E+01
   Dimensionless distance   yplus :  0.12848E-01 0.29637E+01
   Friction thermal sca.    tstar :  0.29508E+00 0.14089E+03
   Rough dim-less th. sca.  tplus :  0.91016E-02 0.20995E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27364E+00       9   0.39114E-05   0.12879E+01 0.19223E+02 
c  Velocity[X]                                      0.54046E+00 
c  Velocity[Y]                                      0.41625E+00 
c  Velocity[Z]                                      0.33115E+00 
c  Pressure     0.97101E-05      14   0.13879E-03   0.96022E-02 0.69738E+01 
c  k            0.79406E-02      11   0.10679E-04   0.22878E-01 0.58360E+02 
c  omega        0.27922E+07       1   0.75044E-07   0.12758E+08 0.57247E+00 
c  TempK        0.97456E+04       6   0.49537E-05   0.60576E+02 0.27949E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6333e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.266          19.239        0.007522        -0.01039
v  Velocity[Y]             -15.781          15.398        0.094616         0.13305
v  Velocity[Z]             -26.044            18.2         -1.6585        -0.51269
v  ǁVelocityǁ         0.00095141          26.216          7.7614          6.7502
v  Pressure                -538.08          213.69          36.297          39.513
v  k                   1.0176e-010          7.2327         0.12159         0.21971
v  omega                    57.518     2.7321e+008     1.2912e+006           76830
v  TempK                    298.24          363.17           330.2          334.02
v  TurbVisc            2.5499e-018      0.00053064     2.9257e-005     9.6258e-005
v  CourantNb            0.00011441          1.5075         0.79784         0.97672
v  FourierNb             0.0036942               1         0.38999         0.11154
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0053809     7.3294e-005      0.00019525

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.72          306.07
v  Yplus               0          2.9637         0.63473         0.49121


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.33831          2.0915          1.1878          1.0883


 INSTANT    0.390000000E-02   TIME STEP NUMBER             390
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924170E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18979E-01 0.47027E+01
   Friction velocity        uk    :  0.18979E-01 0.46986E+01
   Dimensionless distance   yplus :  0.12868E-01 0.29638E+01
   Friction thermal sca.    tstar :  0.30300E+00 0.14067E+03
   Rough dim-less th. sca.  tplus :  0.91158E-02 0.20996E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27371E+00       9   0.39217E-05   0.12881E+01 0.19179E+02 
c  Velocity[X]                                      0.54076E+00 
c  Velocity[Y]                                      0.41130E+00 
c  Velocity[Z]                                      0.33609E+00 
c  Pressure     0.94144E-05      14   0.14058E-03   0.93091E-02 0.67329E+01 
c  k            0.79812E-02      11   0.10667E-04   0.22762E-01 0.57988E+02 
c  omega        0.27922E+07       1   0.73985E-07   0.12778E+08 0.57038E+00 
c  TempK        0.97490E+04       6   0.49233E-05   0.59771E+02 0.27768E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6237e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.267          19.241       0.0074892       -0.010469
v  Velocity[Y]             -15.709          15.407        0.094968          0.1335
v  Velocity[Z]             -26.046          18.835         -1.6588        -0.51273
v  ǁVelocityǁ         0.00095097          26.218          7.7618           6.751
v  Pressure                -537.73          213.71           36.31          39.518
v  k                   1.0176e-010          7.2158         0.12191         0.22072
v  omega                    57.518     2.7321e+008     1.2912e+006           76831
v  TempK                    298.24          363.17          330.24          334.08
v  TurbVisc            2.5499e-018      0.00053321     2.9347e-005     9.6693e-005
v  CourantNb            0.00011483          1.5097         0.79784         0.97672
v  FourierNb             0.0036942               1         0.39006         0.11173
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0053808     7.3289e-005      0.00019524

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.72          306.07
v  Yplus               0          2.9638         0.63477         0.49128


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65413          2.0937          1.1879          1.0885


 INSTANT    0.391000000E-02   TIME STEP NUMBER             391
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924092E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19011E-01 0.47025E+01
   Friction velocity        uk    :  0.19011E-01 0.46985E+01
   Dimensionless distance   yplus :  0.12890E-01 0.29639E+01
   Friction thermal sca.    tstar :  0.31059E+00 0.14043E+03
   Rough dim-less th. sca.  tplus :  0.91311E-02 0.20997E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27378E+00       9   0.39271E-05   0.12675E+01 0.19068E+02 
c  Velocity[X]                                      0.54010E+00 
c  Velocity[Y]                                      0.40378E+00 
c  Velocity[Z]                                      0.32361E+00 
c  Pressure     0.88786E-05      14   0.13571E-03   0.87794E-02 0.62765E+01 
c  k            0.80217E-02      11   0.10689E-04   0.22648E-01 0.57621E+02 
c  omega        0.27922E+07       1   0.71765E-07   0.92158E+07 0.49704E+00 
c  TempK        0.97523E+04       6   0.48924E-05   0.58983E+02 0.27589E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.614e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.267          19.243       0.0074554       -0.010547
v  Velocity[Y]             -15.686          15.415        0.095322         0.13396
v  Velocity[Z]             -26.048          18.656          -1.659        -0.51278
v  ǁVelocityǁ          0.0009507           26.22          7.7623          6.7518
v  Pressure                -537.38          213.72          36.322          39.522
v  k                   1.0176e-010          7.1996         0.12224         0.22172
v  omega                    57.518     2.7321e+008     1.2912e+006           76833
v  TempK                    298.24          363.17          330.28          334.13
v  TurbVisc              2.55e-018      0.00053576     2.9438e-005     9.7127e-005
v  CourantNb            0.00011527           1.512         0.79783         0.97672
v  FourierNb             0.0036943               1         0.39013         0.11193
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0053736     7.3284e-005      0.00019523

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.73          306.07
v  Yplus               0          2.9639         0.63481         0.49135


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6494           2.096           1.188          1.0886


 INSTANT    0.392000000E-02   TIME STEP NUMBER             392
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924186E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19032E-01 0.47024E+01
   Friction velocity        uk    :  0.19032E-01 0.46983E+01
   Dimensionless distance   yplus :  0.12904E-01 0.29640E+01
   Friction thermal sca.    tstar :  0.31586E+00 0.14027E+03
   Rough dim-less th. sca.  tplus :  0.91415E-02 0.20997E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27385E+00       9   0.39403E-05   0.12614E+01 0.18973E+02 
c  Velocity[X]                                      0.53889E+00 
c  Velocity[Y]                                      0.39702E+00 
c  Velocity[Z]                                      0.32545E+00 
c  Pressure     0.90948E-05      14   0.13819E-03   0.89924E-02 0.61800E+01 
c  k            0.80622E-02      11   0.10592E-04   0.22533E-01 0.57256E+02 
c  omega        0.27922E+07       1   0.67952E-07   0.36433E+07 0.35557E+00 
c  TempK        0.97556E+04       6   0.48612E-05   0.58210E+02 0.27413E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.604e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.268          19.245       0.0074196       -0.010625
v  Velocity[Y]             -15.711          15.424        0.095677         0.13441
v  Velocity[Z]             -26.051          19.408         -1.6593        -0.51281
v  ǁVelocityǁ         0.00095048          26.222          7.7627          6.7525
v  Pressure                -537.01          213.73          36.331          39.524
v  k                   1.0177e-010           7.184         0.12256         0.22271
v  omega                    57.518     2.7321e+008     1.2912e+006           76834
v  TempK                    298.24          363.17          330.32          334.19
v  TurbVisc              2.55e-018      0.00053829     2.9528e-005     9.7558e-005
v  CourantNb            0.00011572          1.5142         0.79782         0.97672
v  FourierNb             0.0036946               1          0.3902         0.11212
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0052518     7.3279e-005      0.00019521

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.73          306.07
v  Yplus               0           2.964         0.63484         0.49142


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39498          2.0983           1.188          1.0888


 INSTANT    0.393000000E-02   TIME STEP NUMBER             393
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924275E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19052E-01 0.47022E+01
   Friction velocity        uk    :  0.19051E-01 0.46982E+01
   Dimensionless distance   yplus :  0.12917E-01 0.29641E+01
   Friction thermal sca.    tstar :  0.32140E+00 0.14013E+03
   Rough dim-less th. sca.  tplus :  0.91506E-02 0.20998E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27392E+00       9   0.39519E-05   0.12582E+01 0.18968E+02 
c  Velocity[X]                                      0.53888E+00 
c  Velocity[Y]                                      0.39283E+00 
c  Velocity[Z]                                      0.32648E+00 
c  Pressure     0.91671E-05      14   0.13665E-03   0.90639E-02 0.64839E+01 
c  k            0.81026E-02      11   0.10589E-04   0.22416E-01 0.56894E+02 
c  omega        0.27922E+07       1   0.73016E-07   0.12108E+08 0.55117E+00 
c  TempK        0.97589E+04       6   0.48297E-05   0.57451E+02 0.27239E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5938e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.268          19.247       0.0073838       -0.010702
v  Velocity[Y]             -15.856          15.432        0.096029         0.13487
v  Velocity[Z]             -26.053          19.069         -1.6596        -0.51284
v  ǁVelocityǁ         0.00095045          26.224          7.7631          6.7533
v  Pressure                -536.62          213.74          36.342          39.527
v  k                   1.0177e-010          7.1693         0.12288          0.2237
v  omega                    57.518      2.732e+008     1.2912e+006           76835
v  TempK                    298.24          363.17          330.36          334.25
v  TurbVisc            2.5501e-018       0.0005408     2.9618e-005     9.7988e-005
v  CourantNb            0.00011617          1.5166         0.79782         0.97672
v  FourierNb             0.0036948               1         0.39027         0.11231
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0050803     7.3275e-005       0.0001952

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.74          306.08
v  Yplus               0          2.9641         0.63488         0.49148


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73831          2.1007          1.1881           1.089


 INSTANT    0.394000000E-02   TIME STEP NUMBER             394
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924246E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19057E-01 0.47021E+01
   Friction velocity        uk    :  0.19057E-01 0.46980E+01
   Dimensionless distance   yplus :  0.12921E-01 0.29642E+01
   Friction thermal sca.    tstar :  0.32721E+00 0.14009E+03
   Rough dim-less th. sca.  tplus :  0.91533E-02 0.20999E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27399E+00       9   0.39687E-05   0.12629E+01 0.18985E+02 
c  Velocity[X]                                      0.53968E+00 
c  Velocity[Y]                                      0.39311E+00 
c  Velocity[Z]                                      0.33008E+00 
c  Pressure     0.97174E-05      14   0.13892E-03   0.96069E-02 0.63989E+01 
c  k            0.81429E-02      11   0.10547E-04   0.22307E-01 0.56550E+02 
c  omega        0.27922E+07       1   0.70222E-07   0.10145E+08 0.51600E+00 
c  TempK        0.97622E+04       6   0.47980E-05   0.56708E+02 0.27068E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5841e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.269           19.25       0.0073459       -0.010777
v  Velocity[Y]             -15.832           15.44        0.096385         0.13532
v  Velocity[Z]             -26.055          19.985         -1.6598        -0.51286
v  ǁVelocityǁ         0.00095019          26.227          7.7635           6.754
v  Pressure                -536.22          213.76          36.356          39.533
v  k                   1.0177e-010          7.1554          0.1232         0.22469
v  omega                    57.518      2.732e+008     1.2912e+006           76836
v  TempK                    298.24          363.17          330.39           334.3
v  TurbVisc            2.5501e-018      0.00054328     2.9708e-005     9.8415e-005
v  CourantNb            0.00011659          1.5188         0.79781         0.97672
v  FourierNb             0.0036949               1         0.39034         0.11251
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.004937      7.327e-005      0.00019519

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.74          306.08
v  Yplus               0          2.9642         0.63491         0.49154


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.30362           2.103          1.1881          1.0892


 INSTANT    0.395000000E-02   TIME STEP NUMBER             395
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924334E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19078E-01 0.47019E+01
   Friction velocity        uk    :  0.19078E-01 0.46979E+01
   Dimensionless distance   yplus :  0.12935E-01 0.29643E+01
   Friction thermal sca.    tstar :  0.33329E+00 0.13994E+03
   Rough dim-less th. sca.  tplus :  0.91633E-02 0.20999E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27406E+00       9   0.39793E-05   0.12619E+01 0.18929E+02 
c  Velocity[X]                                      0.53982E+00 
c  Velocity[Y]                                      0.38692E+00 
c  Velocity[Z]                                      0.33519E+00 
c  Pressure     0.92413E-05      14   0.13768E-03   0.91364E-02 0.64318E+01 
c  k            0.81832E-02      11   0.10511E-04   0.22212E-01 0.56229E+02 
c  omega        0.27922E+07       1   0.69465E-07   0.10299E+08 0.52010E+00 
c  TempK        0.97655E+04       6   0.47660E-05   0.55979E+02 0.26900E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.575e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.269          19.252       0.0073089       -0.010852
v  Velocity[Y]             -15.747          15.448        0.096744         0.13577
v  Velocity[Z]             -26.057          19.594         -1.6601        -0.51288
v  ǁVelocityǁ         0.00094985          26.229          7.7639          6.7547
v  Pressure                -535.83          213.77          36.364          39.534
v  k                   1.0177e-010          7.1422         0.12352         0.22567
v  omega                    57.518      2.732e+008     1.2912e+006           76837
v  TempK                    298.24          363.17          330.43          334.36
v  TurbVisc            2.5502e-018      0.00054573     2.9797e-005      9.884e-005
v  CourantNb            0.00011704          1.5209          0.7978         0.97672
v  FourierNb             0.0036948               1         0.39041          0.1127
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0047956     7.3264e-005      0.00019518

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.75          306.08
v  Yplus               0          2.9643         0.63494          0.4916


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9664          2.1052          1.1882          1.0894


 INSTANT    0.396000000E-02   TIME STEP NUMBER             396
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924410E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19106E-01 0.47017E+01
   Friction velocity        uk    :  0.19106E-01 0.46977E+01
   Dimensionless distance   yplus :  0.12954E-01 0.29644E+01
   Friction thermal sca.    tstar :  0.33964E+00 0.13973E+03
   Rough dim-less th. sca.  tplus :  0.91767E-02 0.21000E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27412E+00       9   0.39913E-05   0.12509E+01 0.18907E+02 
c  Velocity[X]                                      0.53978E+00 
c  Velocity[Y]                                      0.38530E+00 
c  Velocity[Z]                                      0.32585E+00 
c  Pressure     0.87376E-05      14   0.13749E-03   0.86377E-02 0.62413E+01 
c  k            0.82234E-02      11   0.10565E-04   0.22120E-01 0.55924E+02 
c  omega        0.27922E+07       1   0.68350E-07   0.90603E+07 0.49190E+00 
c  TempK        0.97687E+04       6   0.47339E-05   0.55266E+02 0.26736E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5659e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.27          19.254       0.0072706       -0.010924
v  Velocity[Y]             -15.705          15.456        0.097108         0.13623
v  Velocity[Z]             -26.059          20.308         -1.6604         -0.5129
v  ǁVelocityǁ         0.00094963           26.23          7.7643          6.7554
v  Pressure                -535.43          213.78           36.37          39.532
v  k                   1.0177e-010          7.1295         0.12384         0.22665
v  omega                    57.518      2.732e+008     1.2912e+006           76838
v  TempK                    298.24          363.17          330.47          334.41
v  TurbVisc            2.5502e-018      0.00054814     2.9886e-005     9.9262e-005
v  CourantNb            0.00011748           1.523         0.79779         0.97671
v  FourierNb             0.0036945               1         0.39048         0.11288
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046808     7.3259e-005      0.00019517

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.75          306.08
v  Yplus               0          2.9644         0.63497         0.49166


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56724          2.1073          1.1883          1.0896


 INSTANT    0.397000000E-02   TIME STEP NUMBER             397
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924503E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19126E-01 0.47015E+01
   Friction velocity        uk    :  0.19126E-01 0.46975E+01
   Dimensionless distance   yplus :  0.12968E-01 0.29644E+01
   Friction thermal sca.    tstar :  0.34512E+00 0.13958E+03
   Rough dim-less th. sca.  tplus :  0.91863E-02 0.21000E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27419E+00       9   0.40016E-05   0.12464E+01 0.18847E+02 
c  Velocity[X]                                      0.53958E+00 
c  Velocity[Y]                                      0.38050E+00 
c  Velocity[Z]                                      0.32630E+00 
c  Pressure     0.85883E-05      14   0.13941E-03   0.84902E-02 0.58397E+01 
c  k            0.82635E-02      11   0.10506E-04   0.22023E-01 0.55623E+02 
c  omega        0.27922E+07       1   0.67907E-07   0.89722E+07 0.49214E+00 
c  TempK        0.97719E+04       6   0.47018E-05   0.54566E+02 0.26574E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5567e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.27          19.256       0.0072303       -0.010995
v  Velocity[Y]             -15.706          15.464        0.097475         0.13669
v  Velocity[Z]              -26.06          19.994         -1.6606        -0.51291
v  ǁVelocityǁ         0.00094948          26.232          7.7646          6.7561
v  Pressure                -535.02          213.78          36.373          39.529
v  k                   1.0177e-010          7.1173         0.12416         0.22762
v  omega                    57.518      2.732e+008     1.2912e+006           76839
v  TempK                    298.25          363.17          330.51          334.47
v  TurbVisc            2.5502e-018      0.00055052     2.9974e-005     9.9683e-005
v  CourantNb            0.00011797          1.5252         0.79778         0.97671
v  FourierNb             0.0036943               1         0.39055         0.11307
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046215     7.3254e-005      0.00019516

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.76          306.08
v  Yplus               0          2.9644         0.63499         0.49172


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63012          2.1095          1.1883          1.0898


 INSTANT    0.398000000E-02   TIME STEP NUMBER             398
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924911E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19141E-01 0.47013E+01
   Friction velocity        uk    :  0.19141E-01 0.46973E+01
   Dimensionless distance   yplus :  0.12978E-01 0.29644E+01
   Friction thermal sca.    tstar :  0.35054E+00 0.13947E+03
   Rough dim-less th. sca.  tplus :  0.91937E-02 0.21000E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27426E+00       9   0.40111E-05   0.12419E+01 0.18793E+02 
c  Velocity[X]                                      0.53807E+00 
c  Velocity[Y]                                      0.37556E+00 
c  Velocity[Z]                                      0.32824E+00 
c  Pressure     0.85043E-05      14   0.14235E-03   0.84065E-02 0.59337E+01 
c  k            0.83035E-02      11   0.10466E-04   0.21918E-01 0.55316E+02 
c  omega        0.27922E+07       1   0.66298E-07   0.67254E+07 0.43492E+00 
c  TempK        0.97751E+04       6   0.46698E-05   0.53879E+02 0.26416E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5473e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.271          19.259       0.0071879       -0.011064
v  Velocity[Y]             -15.804          15.472        0.097841         0.13714
v  Velocity[Z]             -26.062          20.455         -1.6608        -0.51292
v  ǁVelocityǁ         0.00094946          26.233           7.765          6.7568
v  Pressure                 -534.6          213.79          36.373          39.521
v  k                   1.0177e-010          7.1053         0.12448         0.22859
v  omega                    57.518      2.732e+008     1.2912e+006           76840
v  TempK                    298.25          363.17          330.55          334.52
v  TurbVisc            2.5502e-018      0.00055285     3.0063e-005       0.0001001
v  CourantNb            0.00011841          1.5273         0.79777         0.97671
v  FourierNb             0.0036944               1         0.39062         0.11326
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046428     7.3249e-005      0.00019515

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.76          306.09
v  Yplus               0          2.9644         0.63501         0.49177


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60451          2.1117          1.1884            1.09


 INSTANT    0.399000000E-02   TIME STEP NUMBER             399
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925248E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19147E-01 0.47011E+01
   Friction velocity        uk    :  0.19147E-01 0.46971E+01
   Dimensionless distance   yplus :  0.12982E-01 0.29645E+01
   Friction thermal sca.    tstar :  0.35620E+00 0.13943E+03
   Rough dim-less th. sca.  tplus :  0.91964E-02 0.21001E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27432E+00       9   0.40205E-05   0.12422E+01 0.18796E+02 
c  Velocity[X]                                      0.53850E+00 
c  Velocity[Y]                                      0.37480E+00 
c  Velocity[Z]                                      0.32887E+00 
c  Pressure     0.86394E-05      14   0.14334E-03   0.85400E-02 0.60509E+01 
c  k            0.83435E-02      11   0.10537E-04   0.21810E-01 0.54998E+02 
c  omega        0.27922E+07       1   0.69819E-07   0.16915E+08 0.64248E+00 
c  TempK        0.97783E+04       6   0.46377E-05   0.53207E+02 0.26261E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.538e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.271          19.261       0.0071465       -0.011131
v  Velocity[Y]             -15.849          15.479        0.098208          0.1376
v  Velocity[Z]             -26.064          20.316         -1.6611        -0.51292
v  ǁVelocityǁ          0.0009494          26.235          7.7654          6.7575
v  Pressure                -534.17          213.78          36.367          39.508
v  k                   1.0177e-010          7.0937          0.1248         0.22955
v  omega                    57.518     2.7319e+008     1.2912e+006           76841
v  TempK                    298.25          363.17          330.58          334.58
v  TurbVisc            2.5503e-018      0.00055514      3.015e-005      0.00010052
v  CourantNb            0.00011888          1.5295         0.79776         0.97671
v  FourierNb             0.0036945               1         0.39069         0.11344
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046691     7.3244e-005      0.00019513

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.77          306.09
v  Yplus               0          2.9645         0.63504         0.49182


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64334          2.1139          1.1884          1.0902


 INSTANT    0.400000000E-02   TIME STEP NUMBER             400
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925416E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19155E-01 0.47009E+01
   Friction velocity        uk    :  0.19155E-01 0.46969E+01
   Dimensionless distance   yplus :  0.12987E-01 0.29645E+01
   Friction thermal sca.    tstar :  0.36210E+00 0.13937E+03
   Rough dim-less th. sca.  tplus :  0.92002E-02 0.21001E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27439E+00       9   0.40365E-05   0.12434E+01 0.18793E+02 
c  Velocity[X]                                      0.53855E+00 
c  Velocity[Y]                                      0.37531E+00 
c  Velocity[Z]                                      0.32958E+00 
c  Pressure     0.86513E-05      14   0.14530E-03   0.85512E-02 0.60051E+01 
c  k            0.83834E-02      11   0.10575E-04   0.21699E-01 0.54669E+02 
c  omega        0.27922E+07       1   0.65077E-07   0.76360E+07 0.46083E+00 
c  TempK        0.97814E+04       6   0.46058E-05   0.52549E+02 0.26109E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5294e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.272          19.263       0.0071013       -0.011194
v  Velocity[Y]             -15.765          15.486        0.098578         0.13805
v  Velocity[Z]             -26.065          20.456         -1.6613        -0.51292
v  ǁVelocityǁ         0.00094922          26.236          7.7657          6.7581
v  Pressure                -533.74          213.77          36.359          39.494
v  k                   1.0177e-010          7.0824         0.12511         0.23051
v  omega                    57.518     2.7319e+008     1.2912e+006           76842
v  TempK                    298.25          363.17          330.62          334.63
v  TurbVisc            2.5503e-018      0.00055738     3.0238e-005      0.00010093
v  CourantNb            0.00011934          1.5315         0.79775         0.97671
v  FourierNb             0.0036946               1         0.39076         0.11363
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0047109     7.3239e-005      0.00019512

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.77          306.09
v  Yplus               0          2.9645         0.63506         0.49187


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7225           2.116          1.1885          1.0903


 INSTANT    0.401000000E-02   TIME STEP NUMBER             401
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925514E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19173E-01 0.47007E+01
   Friction velocity        uk    :  0.19173E-01 0.46966E+01
   Dimensionless distance   yplus :  0.12999E-01 0.29646E+01
   Friction thermal sca.    tstar :  0.36823E+00 0.13924E+03
   Rough dim-less th. sca.  tplus :  0.92089E-02 0.21001E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27445E+00       9   0.40495E-05   0.12367E+01 0.18693E+02 
c  Velocity[X]                                      0.53779E+00 
c  Velocity[Y]                                      0.36862E+00 
c  Velocity[Z]                                      0.33032E+00 
c  Pressure     0.84070E-05      14   0.14923E-03   0.83096E-02 0.59039E+01 
c  k            0.84232E-02      11   0.10560E-04   0.21581E-01 0.54319E+02 
c  omega        0.27922E+07       1   0.62356E-07   0.34529E+07 0.34352E+00 
c  TempK        0.97846E+04       6   0.45742E-05   0.51905E+02 0.25961E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5211e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.272          19.266       0.0070557       -0.011256
v  Velocity[Y]             -15.717          15.493         0.09895         0.13851
v  Velocity[Z]             -26.067          20.382         -1.6615        -0.51292
v  ǁVelocityǁ         0.00094905          26.238          7.7661          6.7588
v  Pressure                 -533.3          213.76          36.354          39.482
v  k                   1.0177e-010          7.0715         0.12543         0.23146
v  omega                    57.518     2.7319e+008     1.2912e+006           76843
v  TempK                    298.25          363.17          330.66          334.68
v  TurbVisc            2.5503e-018      0.00055956     3.0325e-005      0.00010134
v  CourantNb            0.00011979          1.5335         0.79774          0.9767
v  FourierNb             0.0036947               1         0.39083         0.11381
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0047593     7.3235e-005      0.00019511

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.78          306.09
v  Yplus               0          2.9646         0.63508         0.49191


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49184          2.1179          1.1886          1.0905


 INSTANT    0.402000000E-02   TIME STEP NUMBER             402
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925527E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19189E-01 0.47004E+01
   Friction velocity        uk    :  0.19189E-01 0.46964E+01
   Dimensionless distance   yplus :  0.13010E-01 0.29646E+01
   Friction thermal sca.    tstar :  0.37451E+00 0.13912E+03
   Rough dim-less th. sca.  tplus :  0.92167E-02 0.21002E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27452E+00       9   0.40644E-05   0.12366E+01 0.18691E+02 
c  Velocity[X]                                      0.53728E+00 
c  Velocity[Y]                                      0.36639E+00 
c  Velocity[Z]                                      0.33295E+00 
c  Pressure     0.85558E-05      14   0.15567E-03   0.84564E-02 0.59081E+01 
c  k            0.84628E-02      11   0.10483E-04   0.21448E-01 0.53924E+02 
c  omega        0.27922E+07       1   0.63424E-07   0.55334E+07 0.40349E+00 
c  TempK        0.97877E+04       6   0.45428E-05   0.51276E+02 0.25816E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5127e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.273          19.268        0.007008       -0.011315
v  Velocity[Y]             -15.719            15.5        0.099328         0.13897
v  Velocity[Z]             -26.068          20.363         -1.6617        -0.51291
v  ǁVelocityǁ         0.00084578          26.239          7.7664          6.7594
v  Pressure                -532.85          213.76          36.352          39.472
v  k                   1.0177e-010           7.061         0.12574         0.23241
v  omega                    57.518     2.7319e+008     1.2912e+006           76844
v  TempK                    298.25          363.17          330.69          334.74
v  TurbVisc            2.5503e-018      0.00056168     3.0412e-005      0.00010175
v  CourantNb            0.00012025          1.5355         0.79773          0.9767
v  FourierNb             0.0036949               1          0.3909         0.11399
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.004789     7.3231e-005       0.0001951

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.78          306.09
v  Yplus               0          2.9646          0.6351         0.49196


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49887          2.1199          1.1886          1.0907


 INSTANT    0.403000000E-02   TIME STEP NUMBER             403
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925452E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19198E-01 0.47002E+01
   Friction velocity        uk    :  0.19197E-01 0.46962E+01
   Dimensionless distance   yplus :  0.13016E-01 0.29646E+01
   Friction thermal sca.    tstar :  0.38026E+00 0.13906E+03
   Rough dim-less th. sca.  tplus :  0.92208E-02 0.21002E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27458E+00       9   0.40854E-05   0.12424E+01 0.18752E+02 
c  Velocity[X]                                      0.53874E+00 
c  Velocity[Y]                                      0.36902E+00 
c  Velocity[Z]                                      0.33466E+00 
c  Pressure     0.87447E-05      14   0.16499E-03   0.86432E-02 0.60051E+01 
c  k            0.85024E-02      11   0.10434E-04   0.21302E-01 0.53516E+02 
c  omega        0.27922E+07       1   0.67098E-07   0.14170E+08 0.59178E+00 
c  TempK        0.97908E+04       6   0.45118E-05   0.50661E+02 0.25675E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5042e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.273           19.27       0.0069623       -0.011373
v  Velocity[Y]             -15.806          15.507        0.099707         0.13943
v  Velocity[Z]             -26.069          20.309         -1.6619         -0.5129
v  ǁVelocityǁ         0.00094904           26.24          7.7667            6.76
v  Pressure                -532.39          213.76           36.35          39.464
v  k                   1.0177e-010           7.051         0.12606         0.23336
v  omega                    57.518     2.7319e+008     1.2912e+006           76845
v  TempK                    298.26          363.17          330.73          334.79
v  TurbVisc            2.5503e-018      0.00056375     3.0498e-005      0.00010216
v  CourantNb            0.00012076          1.5375         0.79772          0.9767
v  FourierNb              0.003695               1         0.39097         0.11417
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0048013     7.3227e-005      0.00019509

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.78           306.1
v  Yplus               0          2.9646         0.63512           0.492


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74738           2.122          1.1887          1.0909


 INSTANT    0.404000000E-02   TIME STEP NUMBER             404
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925402E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19198E-01 0.47000E+01
   Friction velocity        uk    :  0.19198E-01 0.46960E+01
   Dimensionless distance   yplus :  0.13016E-01 0.29646E+01
   Friction thermal sca.    tstar :  0.38622E+00 0.13905E+03
   Rough dim-less th. sca.  tplus :  0.92210E-02 0.21001E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27464E+00       9   0.41092E-05   0.12460E+01 0.18727E+02 
c  Velocity[X]                                      0.53965E+00 
c  Velocity[Y]                                      0.36666E+00 
c  Velocity[Z]                                      0.33970E+00 
c  Pressure     0.91754E-05      14   0.15683E-03   0.90684E-02 0.60525E+01 
c  k            0.85419E-02      11   0.10375E-04   0.21165E-01 0.53131E+02 
c  omega        0.27922E+07       1   0.66988E-07   0.14157E+08 0.58943E+00 
c  TempK        0.97938E+04       6   0.44812E-05   0.50059E+02 0.25538E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4958e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.274          19.272        0.006915       -0.011427
v  Velocity[Y]             -15.865          15.513         0.10008         0.13989
v  Velocity[Z]              -26.07          20.226         -1.6621        -0.51289
v  ǁVelocityǁ          0.0008955           26.24           7.767          6.7607
v  Pressure                -531.92          213.76          36.347          39.454
v  k                   1.0177e-010          7.0414         0.12637          0.2343
v  omega                    57.517     2.7319e+008     1.2912e+006           76846
v  TempK                    298.26          363.17          330.77          334.84
v  TurbVisc            2.5503e-018      0.00056574     3.0584e-005      0.00010256
v  CourantNb            0.00012124          1.5395          0.7977         0.97669
v  FourierNb              0.003695               1         0.39104         0.11435
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0047442     7.3223e-005      0.00019508

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.79           306.1
v  Yplus               0          2.9646         0.63514         0.49205


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61486           2.124          1.1887           1.091


 INSTANT    0.405000000E-02   TIME STEP NUMBER             405
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925604E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19195E-01 0.46997E+01
   Friction velocity        uk    :  0.19195E-01 0.46957E+01
   Dimensionless distance   yplus :  0.13015E-01 0.29646E+01
   Friction thermal sca.    tstar :  0.39238E+00 0.13907E+03
   Rough dim-less th. sca.  tplus :  0.92197E-02 0.21001E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27471E+00       9   0.41227E-05   0.12512E+01 0.18699E+02 
c  Velocity[X]                                      0.53946E+00 
c  Velocity[Y]                                      0.36560E+00 
c  Velocity[Z]                                      0.34615E+00 
c  Pressure     0.88683E-05      14   0.14792E-03   0.87647E-02 0.63957E+01 
c  k            0.85814E-02      11   0.10303E-04   0.21064E-01 0.52823E+02 
c  omega        0.27922E+07       1   0.62958E-07   0.83549E+07 0.47190E+00 
c  TempK        0.97969E+04       6   0.44510E-05   0.49465E+02 0.25402E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.488e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.275          19.274       0.0068669       -0.011479
v  Velocity[Y]             -15.806          15.519         0.10046         0.14036
v  Velocity[Z]             -26.071          20.187         -1.6623        -0.51287
v  ǁVelocityǁ         0.00094901          26.241          7.7673          6.7613
v  Pressure                -531.45          213.74          36.333          39.434
v  k                   1.0177e-010          7.0323         0.12668         0.23523
v  omega                    57.517     2.7319e+008     1.2912e+006           76847
v  TempK                    298.26          363.17           330.8           334.9
v  TurbVisc            2.5502e-018      0.00056766      3.067e-005      0.00010296
v  CourantNb            0.00012171          1.5413         0.79769         0.97669
v  FourierNb             0.0036951               1         0.39111         0.11453
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046945     7.3219e-005      0.00019507

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.79           306.1
v  Yplus               0          2.9646         0.63515         0.49209


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78055          2.1259          1.1888          1.0912


 INSTANT    0.406000000E-02   TIME STEP NUMBER             406
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925613E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19207E-01 0.46995E+01
   Friction velocity        uk    :  0.19207E-01 0.46955E+01
   Dimensionless distance   yplus :  0.13023E-01 0.29646E+01
   Friction thermal sca.    tstar :  0.39875E+00 0.13899E+03
   Rough dim-less th. sca.  tplus :  0.92253E-02 0.21001E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27477E+00       9   0.41370E-05   0.12371E+01 0.18572E+02 
c  Velocity[X]                                      0.53890E+00 
c  Velocity[Y]                                      0.35914E+00 
c  Velocity[Z]                                      0.33907E+00 
c  Pressure     0.87728E-05      14   0.14874E-03   0.86703E-02 0.61203E+01 
c  k            0.86207E-02      11   0.10327E-04   0.21003E-01 0.52598E+02 
c  omega        0.27922E+07       1   0.59415E-07   0.32342E+07 0.32667E+00 
c  TempK        0.97999E+04       6   0.44213E-05   0.48883E+02 0.25269E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4808e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.276          19.276       0.0068177       -0.011527
v  Velocity[Y]             -15.757          15.525         0.10084         0.14082
v  Velocity[Z]             -26.071          20.093         -1.6624        -0.51285
v  ǁVelocityǁ         0.00094891          26.242          7.7676          6.7618
v  Pressure                -530.96          213.74          36.324          39.419
v  k                   1.0177e-010          7.0237         0.12699         0.23616
v  omega                    57.517     2.7318e+008     1.2912e+006           76848
v  TempK                    298.26          363.17          330.84          334.95
v  TurbVisc            2.5502e-018      0.00056949     3.0756e-005      0.00010336
v  CourantNb            0.00012219           1.543         0.79768         0.97669
v  FourierNb             0.0036952               1         0.39118          0.1147
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046524     7.3215e-005      0.00019506

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           304.8           306.1
v  Yplus               0          2.9646         0.63516         0.49213


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82373          2.1276          1.1889          1.0914


 INSTANT    0.407000000E-02   TIME STEP NUMBER             407
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925693E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19217E-01 0.46992E+01
   Friction velocity        uk    :  0.19217E-01 0.46952E+01
   Dimensionless distance   yplus :  0.13029E-01 0.29646E+01
   Friction thermal sca.    tstar :  0.40532E+00 0.13892E+03
   Rough dim-less th. sca.  tplus :  0.92301E-02 0.21001E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27483E+00       9   0.41529E-05   0.12397E+01 0.18541E+02 
c  Velocity[X]                                      0.53927E+00 
c  Velocity[Y]                                      0.35710E+00 
c  Velocity[Z]                                      0.34334E+00 
c  Pressure     0.90320E-05      14   0.14904E-03   0.89265E-02 0.60956E+01 
c  k            0.86599E-02      11   0.10334E-04   0.20906E-01 0.52294E+02 
c  omega        0.27922E+07       1   0.58461E-07   0.26980E+07 0.30815E+00 
c  TempK        0.98029E+04       6   0.43921E-05   0.48310E+02 0.25137E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4735e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.276          19.277       0.0067683       -0.011573
v  Velocity[Y]             -15.753           15.53         0.10122         0.14129
v  Velocity[Z]             -26.072          20.069         -1.6626        -0.51283
v  ǁVelocityǁ         0.00094894          26.243          7.7679          6.7624
v  Pressure                -530.47          213.73          36.316          39.405
v  k                   1.0177e-010          7.0157          0.1273         0.23709
v  omega                    57.517     2.7318e+008     1.2912e+006           76849
v  TempK                    298.26          363.17          330.88             335
v  TurbVisc            2.5502e-018      0.00057121     3.0841e-005      0.00010376
v  CourantNb            0.00012267          1.5448         0.79767         0.97668
v  FourierNb             0.0036953               1         0.39125         0.11488
v  total_pressure      1.0079e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046212     7.3211e-005      0.00019505

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           304.8           306.1
v  Yplus               0          2.9646         0.63518         0.49217


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53385          2.1294          1.1889          1.0916


 INSTANT    0.408000000E-02   TIME STEP NUMBER             408
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925655E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19218E-01 0.46990E+01
   Friction velocity        uk    :  0.19218E-01 0.46950E+01
   Dimensionless distance   yplus :  0.13030E-01 0.29646E+01
   Friction thermal sca.    tstar :  0.41209E+00 0.13891E+03
   Rough dim-less th. sca.  tplus :  0.92306E-02 0.21001E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27490E+00       9   0.41677E-05   0.12378E+01 0.18551E+02 
c  Velocity[X]                                      0.53908E+00 
c  Velocity[Y]                                      0.35571E+00 
c  Velocity[Z]                                      0.34302E+00 
c  Pressure     0.86764E-05      14   0.14982E-03   0.85748E-02 0.61368E+01 
c  k            0.86990E-02      11   0.10348E-04   0.20803E-01 0.51972E+02 
c  omega        0.27922E+07       1   0.61632E-07   0.76597E+07 0.44792E+00 
c  TempK        0.98059E+04       6   0.43634E-05   0.47748E+02 0.25009E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.466e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.277          19.279       0.0067209       -0.011615
v  Velocity[Y]             -15.834          15.536         0.10161         0.14175
v  Velocity[Z]             -26.073          19.977         -1.6628         -0.5128
v  ǁVelocityǁ         0.00094909          26.243          7.7682           6.763
v  Pressure                -529.96          213.73           36.31          39.392
v  k                   1.0177e-010          7.0082         0.12761         0.23801
v  omega                    57.517     2.7318e+008     1.2912e+006           76850
v  TempK                    298.26          363.17          330.91          335.06
v  TurbVisc            2.5502e-018      0.00057282     3.0926e-005      0.00010415
v  CourantNb            0.00012317          1.5466         0.79766         0.97668
v  FourierNb             0.0036954               1         0.39132         0.11505
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046029     7.3206e-005      0.00019504

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.81          306.11
v  Yplus               0          2.9646         0.63519         0.49221


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0001          2.1312           1.189          1.0917


 INSTANT    0.409000000E-02   TIME STEP NUMBER             409
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925535E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19209E-01 0.46987E+01
   Friction velocity        uk    :  0.19209E-01 0.46947E+01
   Dimensionless distance   yplus :  0.13024E-01 0.29646E+01
   Friction thermal sca.    tstar :  0.41905E+00 0.13897E+03
   Rough dim-less th. sca.  tplus :  0.92265E-02 0.21001E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27496E+00       9   0.41834E-05   0.12498E+01 0.18636E+02 
c  Velocity[X]                                      0.54099E+00 
c  Velocity[Y]                                      0.36066E+00 
c  Velocity[Z]                                      0.34817E+00 
c  Pressure     0.92981E-05      14   0.15171E-03   0.91888E-02 0.62196E+01 
c  k            0.87380E-02      11   0.10285E-04   0.20684E-01 0.51618E+02 
c  omega        0.27922E+07       1   0.66644E-07   0.18988E+08 0.67089E+00 
c  TempK        0.98089E+04       6   0.43355E-05   0.47199E+02 0.24883E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4585e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.278           19.28       0.0066759       -0.011653
v  Velocity[Y]              -15.89           15.54         0.10199         0.14222
v  Velocity[Z]             -26.073          19.893         -1.6629        -0.51278
v  ǁVelocityǁ         0.00094923          26.243          7.7685          6.7636
v  Pressure                -529.44          213.72          36.306          39.382
v  k                   1.0176e-010          7.0012         0.12792         0.23893
v  omega                    57.517     2.7318e+008     1.2912e+006           76851
v  TempK                    298.27          363.17          330.95          335.11
v  TurbVisc            2.5501e-018      0.00057433      3.101e-005      0.00010454
v  CourantNb             0.0001237          1.5483         0.79764         0.97667
v  FourierNb             0.0036955               1         0.39139         0.11523
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045915     7.3202e-005      0.00019503

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.81          306.11
v  Yplus               0          2.9646         0.63521         0.49225


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44573           2.133           1.189          1.0919


 INSTANT    0.410000000E-02   TIME STEP NUMBER             410
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925541E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19200E-01 0.46984E+01
   Friction velocity        uk    :  0.19200E-01 0.46944E+01
   Dimensionless distance   yplus :  0.13018E-01 0.29645E+01
   Friction thermal sca.    tstar :  0.42621E+00 0.13904E+03
   Rough dim-less th. sca.  tplus :  0.92220E-02 0.21001E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27502E+00       9   0.42005E-05   0.12599E+01 0.18613E+02 
c  Velocity[X]                                      0.54203E+00 
c  Velocity[Y]                                      0.35980E+00 
c  Velocity[Z]                                      0.35807E+00 
c  Pressure     0.89788E-05      15   0.15212E-03   0.88730E-02 0.68904E+01 
c  k            0.87769E-02      11   0.10252E-04   0.20573E-01 0.51280E+02 
c  omega        0.27922E+07       1   0.62547E-07   0.11203E+08 0.53320E+00 
c  TempK        0.98119E+04       6   0.43082E-05   0.46659E+02 0.24758E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4517e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.279          19.282       0.0066305       -0.011689
v  Velocity[Y]             -15.827          15.545         0.10238         0.14269
v  Velocity[Z]             -26.073          19.451         -1.6631        -0.51275
v  ǁVelocityǁ         0.00094922          26.243          7.7688          6.7641
v  Pressure                -528.93           213.7          36.286          39.356
v  k                   1.0176e-010          6.9947         0.12823         0.23985
v  omega                    57.516     2.7318e+008     1.2912e+006           76852
v  TempK                    298.27          363.17          330.98          335.16
v  TurbVisc            2.5501e-018      0.00057574     3.1095e-005      0.00010493
v  CourantNb            0.00012416            1.55         0.79763         0.97667
v  FourierNb             0.0036956               1         0.39146          0.1154
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045616     7.3198e-005      0.00019502

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.82          306.11
v  Yplus               0          2.9645         0.63522         0.49229


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.89622          2.1346          1.1891          1.0921


 INSTANT    0.411000000E-02   TIME STEP NUMBER             411
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925547E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19203E-01 0.46982E+01
   Friction velocity        uk    :  0.19203E-01 0.46942E+01
   Dimensionless distance   yplus :  0.13020E-01 0.29644E+01
   Friction thermal sca.    tstar :  0.43356E+00 0.13901E+03
   Rough dim-less th. sca.  tplus :  0.92235E-02 0.21000E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27508E+00       9   0.42168E-05   0.12411E+01 0.18450E+02 
c  Velocity[X]                                      0.54190E+00 
c  Velocity[Y]                                      0.35271E+00 
c  Velocity[Z]                                      0.34651E+00 
c  Pressure     0.89104E-05      15   0.15436E-03   0.88050E-02 0.68056E+01 
c  k            0.88157E-02      11   0.10205E-04   0.20471E-01 0.50958E+02 
c  omega        0.27922E+07       1   0.57312E-07   0.33295E+07 0.33351E+00 
c  TempK        0.98148E+04       6   0.42815E-05   0.46130E+02 0.24636E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4454e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.279          19.283       0.0065851        -0.01172
v  Velocity[Y]             -15.776          15.549         0.10277         0.14316
v  Velocity[Z]             -26.073          19.738         -1.6632        -0.51271
v  ǁVelocityǁ         0.00094921          26.243           7.769          6.7647
v  Pressure                -528.43          213.68          36.264          39.328
v  k                   1.0176e-010          6.9887         0.12854         0.24075
v  omega                    57.516     2.7318e+008     1.2912e+006           76853
v  TempK                    298.27          363.17          331.02          335.21
v  TurbVisc              2.55e-018      0.00057704     3.1179e-005      0.00010532
v  CourantNb            0.00012469          1.5515         0.79762         0.97666
v  FourierNb             0.0036957               1         0.39153         0.11557
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045169     7.3193e-005      0.00019501

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.82          306.11
v  Yplus               0          2.9644         0.63522         0.49232


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77361          2.1361          1.1891          1.0922


 INSTANT    0.412000000E-02   TIME STEP NUMBER             412
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925415E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19206E-01 0.46979E+01
   Friction velocity        uk    :  0.19206E-01 0.46939E+01
   Dimensionless distance   yplus :  0.13022E-01 0.29644E+01
   Friction thermal sca.    tstar :  0.44109E+00 0.13899E+03
   Rough dim-less th. sca.  tplus :  0.92247E-02 0.21000E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27514E+00       9   0.42443E-05   0.12480E+01 0.18431E+02 
c  Velocity[X]                                      0.54395E+00 
c  Velocity[Y]                                      0.35159E+00 
c  Velocity[Z]                                      0.35243E+00 
c  Pressure     0.93784E-05      15   0.15785E-03   0.92674E-02 0.64450E+01 
c  k            0.88544E-02      11   0.10203E-04   0.20386E-01 0.50661E+02 
c  omega        0.27922E+07       1   0.56382E-07   0.25555E+07 0.31015E+00 
c  TempK        0.98178E+04       6   0.42556E-05   0.45610E+02 0.24516E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4391e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.28          19.285       0.0065387       -0.011749
v  Velocity[Y]              -15.77          15.553         0.10315         0.14364
v  Velocity[Z]             -26.073          18.532         -1.6634        -0.51268
v  ǁVelocityǁ         0.00094932          26.243          7.7693          6.7652
v  Pressure                -527.92          213.67          36.245          39.304
v  k                   1.0176e-010          6.9832         0.12884         0.24166
v  omega                    57.516     2.7318e+008     1.2912e+006           76853
v  TempK                    298.27          363.17          331.05          335.26
v  TurbVisc            2.5499e-018      0.00057826     3.1262e-005      0.00010571
v  CourantNb            0.00012516           1.553          0.7976         0.97666
v  FourierNb             0.0036959               1          0.3916         0.11574
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044667     7.3189e-005        0.000195

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.83          306.11
v  Yplus               0          2.9644         0.63523         0.49236


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.32744          2.1377          1.1892          1.0924


 INSTANT    0.413000000E-02   TIME STEP NUMBER             413
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925480E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19200E-01 0.46976E+01
   Friction velocity        uk    :  0.19200E-01 0.46936E+01
   Dimensionless distance   yplus :  0.13018E-01 0.29643E+01
   Friction thermal sca.    tstar :  0.44880E+00 0.13903E+03
   Rough dim-less th. sca.  tplus :  0.92219E-02 0.20999E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27521E+00       9   0.42706E-05   0.12496E+01 0.18431E+02 
c  Velocity[X]                                      0.54641E+00 
c  Velocity[Y]                                      0.35102E+00 
c  Velocity[Z]                                      0.35215E+00 
c  Pressure     0.94280E-05      14   0.15966E-03   0.93158E-02 0.63319E+01 
c  k            0.88930E-02      11   0.10231E-04   0.20306E-01 0.50377E+02 
c  omega        0.27922E+07       1   0.57759E-07   0.48544E+07 0.38180E+00 
c  TempK        0.98207E+04       6   0.42303E-05   0.45101E+02 0.24398E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4326e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.28          19.286       0.0064924       -0.011774
v  Velocity[Y]              -15.85          15.556         0.10354         0.14411
v  Velocity[Z]             -26.073          19.437         -1.6635        -0.51264
v  ǁVelocityǁ         0.00094954          26.243          7.7695          6.7657
v  Pressure                 -527.4          213.66           36.23          39.283
v  k                   1.0175e-010          6.9781         0.12915         0.24256
v  omega                    57.516     2.7317e+008     1.2912e+006           76854
v  TempK                    298.28          363.17          331.09          335.31
v  TurbVisc            2.5498e-018      0.00057937     3.1346e-005      0.00010609
v  CourantNb            0.00012565          1.5546         0.79759         0.97666
v  FourierNb              0.003696               1         0.39167         0.11591
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044135     7.3185e-005      0.00019499

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.83          306.12
v  Yplus               0          2.9643         0.63524         0.49239


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59596          2.1393          1.1893          1.0926


 INSTANT    0.414000000E-02   TIME STEP NUMBER             414
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925613E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19184E-01 0.46973E+01
   Friction velocity        uk    :  0.19184E-01 0.46933E+01
   Dimensionless distance   yplus :  0.13007E-01 0.29643E+01
   Friction thermal sca.    tstar :  0.45669E+00 0.13915E+03
   Rough dim-less th. sca.  tplus :  0.92142E-02 0.20999E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27527E+00       9   0.42939E-05   0.12624E+01 0.18495E+02 
c  Velocity[X]                                      0.54860E+00 
c  Velocity[Y]                                      0.35312E+00 
c  Velocity[Z]                                      0.36064E+00 
c  Pressure     0.98152E-05      14   0.16263E-03   0.96981E-02 0.64911E+01 
c  k            0.89315E-02      11   0.10273E-04   0.20232E-01 0.50106E+02 
c  omega        0.27922E+07       1   0.62078E-07   0.12498E+08 0.55679E+00 
c  TempK        0.98236E+04       6   0.42058E-05   0.44601E+02 0.24281E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4261e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.281          19.288       0.0064458       -0.011797
v  Velocity[Y]             -15.908          15.559         0.10393         0.14459
v  Velocity[Z]             -26.073          18.623         -1.6637        -0.51261
v  ǁVelocityǁ         0.00094979          26.243          7.7698          6.7662
v  Pressure                -526.86          213.64          36.215          39.262
v  k                   1.0175e-010          6.9734         0.12945         0.24346
v  omega                    57.516     2.7317e+008     1.2912e+006           76855
v  TempK                    298.28          363.17          331.12          335.37
v  TurbVisc            2.5497e-018      0.00058036     3.1429e-005      0.00010647
v  CourantNb            0.00012613          1.5562         0.79758         0.97665
v  FourierNb             0.0036962               1         0.39174         0.11608
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0043588      7.318e-005      0.00019498

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.83          306.12
v  Yplus               0          2.9643         0.63525         0.49242


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.27513          2.1408          1.1893          1.0927


 INSTANT    0.415000000E-02   TIME STEP NUMBER             415
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925640E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19165E-01 0.46971E+01
   Friction velocity        uk    :  0.19165E-01 0.46931E+01
   Dimensionless distance   yplus :  0.12994E-01 0.29642E+01
   Friction thermal sca.    tstar :  0.46475E+00 0.13929E+03
   Rough dim-less th. sca.  tplus :  0.92052E-02 0.20998E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27533E+00       9   0.43180E-05   0.12795E+01 0.18602E+02 
c  Velocity[X]                                      0.55181E+00 
c  Velocity[Y]                                      0.36010E+00 
c  Velocity[Z]                                      0.36762E+00 
c  Pressure     0.96681E-05      15   0.16251E-03   0.95527E-02 0.72647E+01 
c  k            0.89700E-02      11   0.10311E-04   0.20169E-01 0.49857E+02 
c  omega        0.27922E+07       1   0.62048E-07   0.13489E+08 0.57811E+00 
c  TempK        0.98265E+04       6   0.41820E-05   0.44109E+02 0.24165E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4204e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.281          19.289          0.0064       -0.011817
v  Velocity[Y]             -15.844          15.562         0.10432         0.14507
v  Velocity[Z]             -26.073          19.037         -1.6638        -0.51257
v  ǁVelocityǁ         0.00094985          26.243            7.77          6.7667
v  Pressure                -526.33          213.63          36.193          39.234
v  k                   1.0174e-010          6.9692         0.12976         0.24435
v  omega                    57.515     2.7317e+008     1.2912e+006           76856
v  TempK                    298.28          363.17          331.16          335.42
v  TurbVisc            2.5497e-018      0.00058126     3.1511e-005      0.00010685
v  CourantNb            0.00012661          1.5575         0.79756         0.97665
v  FourierNb             0.0036964               1         0.39181         0.11625
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0043039     7.3175e-005      0.00019497

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.84          306.12
v  Yplus               0          2.9642         0.63526         0.49245


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6824          2.1422          1.1894          1.0929


 INSTANT    0.416000000E-02   TIME STEP NUMBER             416
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925466E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19161E-01 0.46968E+01
   Friction velocity        uk    :  0.19161E-01 0.46928E+01
   Dimensionless distance   yplus :  0.12992E-01 0.29640E+01
   Friction thermal sca.    tstar :  0.47296E+00 0.13931E+03
   Rough dim-less th. sca.  tplus :  0.92034E-02 0.20997E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27539E+00       9   0.43405E-05   0.12656E+01 0.18465E+02 
c  Velocity[X]                                      0.55349E+00 
c  Velocity[Y]                                      0.35379E+00 
c  Velocity[Z]                                      0.35835E+00 
c  Pressure     0.92855E-05      15   0.16118E-03   0.91750E-02 0.67503E+01 
c  k            0.90083E-02      11   0.10303E-04   0.20109E-01 0.49614E+02 
c  omega        0.27922E+07       1   0.58800E-07   0.80986E+07 0.46295E+00 
c  TempK        0.98293E+04       6   0.41589E-05   0.43627E+02 0.24051E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4152e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.282           19.29       0.0063518       -0.011834
v  Velocity[Y]             -15.791          15.564         0.10471         0.14555
v  Velocity[Z]             -26.072          17.485         -1.6639        -0.51253
v  ǁVelocityǁ         0.00094991          26.242          7.7702          6.7672
v  Pressure                 -525.8           213.6           36.17          39.207
v  k                   1.0174e-010          6.9652         0.13006         0.24524
v  omega                    57.515     2.7317e+008     1.2912e+006           76857
v  TempK                    298.28          363.17          331.19          335.47
v  TurbVisc            2.5495e-018      0.00058205     3.1594e-005      0.00010722
v  CourantNb            0.00012715          1.5588         0.79755         0.97664
v  FourierNb             0.0036966               1         0.39188         0.11641
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.004251      7.317e-005      0.00019496

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.84          306.12
v  Yplus               0           2.964         0.63527         0.49249


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6684          2.1435          1.1894          1.0931


 INSTANT    0.417000000E-02   TIME STEP NUMBER             417
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925756E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19157E-01 0.46965E+01
   Friction velocity        uk    :  0.19157E-01 0.46925E+01
   Dimensionless distance   yplus :  0.12989E-01 0.29639E+01
   Friction thermal sca.    tstar :  0.48133E+00 0.13934E+03
   Rough dim-less th. sca.  tplus :  0.92015E-02 0.20997E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27545E+00       9   0.43700E-05   0.12685E+01 0.18415E+02 
c  Velocity[X]                                      0.55630E+00 
c  Velocity[Y]                                      0.35166E+00 
c  Velocity[Z]                                      0.36056E+00 
c  Pressure     0.94309E-05      16   0.16445E-03   0.93184E-02 0.83089E+01 
c  k            0.90465E-02      11   0.10296E-04   0.20062E-01 0.49386E+02 
c  omega        0.27922E+07       1   0.55078E-07   0.33741E+07 0.33471E+00 
c  TempK        0.98322E+04       6   0.41365E-05   0.43155E+02 0.23938E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step       6.41e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.282          19.291       0.0063027       -0.011848
v  Velocity[Y]             -15.783          15.566          0.1051         0.14604
v  Velocity[Z]             -26.071          18.733          -1.664        -0.51248
v  ǁVelocityǁ         0.00095017          26.241          7.7704          6.7677
v  Pressure                -525.28          213.57          36.133          39.164
v  k                   1.0173e-010          6.9617         0.13037         0.24612
v  omega                    57.515     2.7317e+008     1.2912e+006           76857
v  TempK                    298.28          363.17          331.23          335.52
v  TurbVisc            2.5494e-018      0.00058275     3.1676e-005       0.0001076
v  CourantNb             0.0001276          1.5601         0.79754         0.97664
v  FourierNb             0.0036968               1         0.39194         0.11658
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.004199     7.3165e-005      0.00019495

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.85          306.12
v  Yplus               0          2.9639         0.63527         0.49252


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44557          2.1448          1.1895          1.0932


 INSTANT    0.418000000E-02   TIME STEP NUMBER             418
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925332E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19139E-01 0.46962E+01
   Friction velocity        uk    :  0.19139E-01 0.46922E+01
   Dimensionless distance   yplus :  0.12977E-01 0.29638E+01
   Friction thermal sca.    tstar :  0.48985E+00 0.13947E+03
   Rough dim-less th. sca.  tplus :  0.91928E-02 0.20996E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27551E+00       9   0.43858E-05   0.12750E+01 0.18445E+02 
c  Velocity[X]                                      0.55977E+00 
c  Velocity[Y]                                      0.35207E+00 
c  Velocity[Z]                                      0.36320E+00 
c  Pressure     0.96818E-05      16   0.17341E-03   0.95661E-02 0.66224E+01 
c  k            0.90846E-02      11   0.10341E-04   0.20015E-01 0.49159E+02 
c  omega        0.27922E+07       1   0.56380E-07   0.50553E+07 0.38306E+00 
c  TempK        0.98350E+04       6   0.41148E-05   0.42691E+02 0.23826E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4046e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.282          19.293       0.0062522       -0.011861
v  Velocity[Y]             -15.874          15.567         0.10549         0.14652
v  Velocity[Z]              -26.07          18.539         -1.6642        -0.51244
v  ǁVelocityǁ         0.00095049           26.24          7.7706          6.7682
v  Pressure                -524.73          213.55          36.113          39.139
v  k                   1.0173e-010          6.9585         0.13067           0.247
v  omega                    57.515     2.7317e+008     1.2912e+006           76858
v  TempK                    298.29          363.17          331.26          335.57
v  TurbVisc            2.5493e-018      0.00058336     3.1758e-005      0.00010797
v  CourantNb            0.00012814          1.5614         0.79752         0.97663
v  FourierNb             0.0036971               1         0.39201         0.11674
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0041365      7.316e-005      0.00019494

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.85          306.13
v  Yplus               0          2.9638         0.63528         0.49255


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47631          2.1461          1.1895          1.0934


 INSTANT    0.419000000E-02   TIME STEP NUMBER             419
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925472E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19114E-01 0.46959E+01
   Friction velocity        uk    :  0.19114E-01 0.46919E+01
   Dimensionless distance   yplus :  0.12960E-01 0.29637E+01
   Friction thermal sca.    tstar :  0.49849E+00 0.13966E+03
   Rough dim-less th. sca.  tplus :  0.91807E-02 0.20995E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27557E+00       9   0.44013E-05   0.12846E+01 0.18492E+02 
c  Velocity[X]                                      0.56160E+00 
c  Velocity[Y]                                      0.35479E+00 
c  Velocity[Z]                                      0.36825E+00 
c  Pressure     0.94979E-05      15   0.16776E-03   0.93844E-02 0.69559E+01 
c  k            0.91226E-02      11   0.10360E-04   0.19961E-01 0.48926E+02 
c  omega        0.27922E+07       1   0.60974E-07   0.14165E+08 0.58895E+00 
c  TempK        0.98378E+04       6   0.40938E-05   0.42233E+02 0.23714E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3993e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.283          19.294       0.0062033       -0.011871
v  Velocity[Y]             -15.927          15.568         0.10588         0.14701
v  Velocity[Z]              -26.07          17.583         -1.6643        -0.51239
v  ǁVelocityǁ         0.00095081          26.239          7.7709          6.7686
v  Pressure                -524.17          213.53          36.091          39.112
v  k                   1.0172e-010          6.9557         0.13098         0.24788
v  omega                    57.514     2.7317e+008     1.2912e+006           76859
v  TempK                    298.29          363.17          331.29          335.62
v  TurbVisc            2.5492e-018      0.00058386     3.1839e-005      0.00010834
v  CourantNb            0.00012859          1.5627         0.79751         0.97663
v  FourierNb             0.0036973               1         0.39208         0.11691
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.004069     7.3155e-005      0.00019493

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.86          306.13
v  Yplus               0          2.9637         0.63529         0.49258


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43953          2.1474          1.1896          1.0935


 INSTANT    0.420000000E-02   TIME STEP NUMBER             420
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925561E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19089E-01 0.46957E+01
   Friction velocity        uk    :  0.19089E-01 0.46917E+01
   Dimensionless distance   yplus :  0.12943E-01 0.29636E+01
   Friction thermal sca.    tstar :  0.50727E+00 0.13984E+03
   Rough dim-less th. sca.  tplus :  0.91686E-02 0.20994E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27563E+00       9   0.44221E-05   0.12939E+01 0.18552E+02 
c  Velocity[X]                                      0.56370E+00 
c  Velocity[Y]                                      0.35797E+00 
c  Velocity[Z]                                      0.37228E+00 
c  Pressure     0.98311E-05      15   0.16795E-03   0.97137E-02 0.72355E+01 
c  k            0.91606E-02      11   0.10402E-04   0.19920E-01 0.48711E+02 
c  omega        0.27922E+07       1   0.58688E-07   0.96586E+07 0.49850E+00 
c  TempK        0.98406E+04       6   0.40734E-05   0.41784E+02 0.23604E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3948e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.283          19.295       0.0061516       -0.011877
v  Velocity[Y]             -15.855          15.568         0.10627          0.1475
v  Velocity[Z]             -26.069           17.87         -1.6644        -0.51235
v  ǁVelocityǁ          0.0009509          26.238          7.7711          6.7691
v  Pressure                -523.61          213.51          36.065          39.081
v  k                   1.0172e-010          6.9532         0.13128         0.24875
v  omega                    57.514     2.7317e+008     1.2912e+006           76860
v  TempK                    298.29          363.17          331.33          335.67
v  TurbVisc             2.549e-018      0.00058428      3.192e-005       0.0001087
v  CourantNb            0.00012905          1.5638          0.7975         0.97663
v  FourierNb             0.0036976               1         0.39215         0.11707
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039995      7.315e-005      0.00019492

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.86          306.13
v  Yplus               0          2.9636         0.63529         0.49261


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63861          2.1485          1.1897          1.0937


 INSTANT    0.421000000E-02   TIME STEP NUMBER             421
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925763E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19083E-01 0.46954E+01
   Friction velocity        uk    :  0.19083E-01 0.46914E+01
   Dimensionless distance   yplus :  0.12939E-01 0.29635E+01
   Friction thermal sca.    tstar :  0.51618E+00 0.13988E+03
   Rough dim-less th. sca.  tplus :  0.91659E-02 0.20994E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27569E+00       9   0.44506E-05   0.13039E+01 0.18559E+02 
c  Velocity[X]                                      0.56677E+00 
c  Velocity[Y]                                      0.35797E+00 
c  Velocity[Z]                                      0.37914E+00 
c  Pressure     0.10562E-04      16   0.17257E-03   0.10436E-01 0.79629E+01 
c  k            0.91984E-02      11   0.10526E-04   0.19882E-01 0.48501E+02 
c  omega        0.27922E+07       1   0.58093E-07   0.90729E+07 0.48311E+00 
c  TempK        0.98434E+04       6   0.40538E-05   0.41343E+02 0.23494E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3909e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.283          19.297       0.0061001       -0.011881
v  Velocity[Y]             -15.803          15.567         0.10666         0.14799
v  Velocity[Z]             -26.067          16.403         -1.6645         -0.5123
v  ǁVelocityǁ         0.00095103          26.237          7.7712          6.7695
v  Pressure                -523.06          213.48          36.035          39.046
v  k                   1.0171e-010          6.9511         0.13158         0.24962
v  omega                    57.514     2.7317e+008     1.2912e+006           76860
v  TempK                    298.29          363.17          331.36          335.72
v  TurbVisc            2.5489e-018      0.00058459     3.2001e-005      0.00010907
v  CourantNb             0.0001296          1.5647         0.79748         0.97662
v  FourierNb             0.0036979               1         0.39223         0.11723
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039291     7.3145e-005      0.00019491

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.86          306.13
v  Yplus               0          2.9635          0.6353         0.49264


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.3079          2.1494          1.1897          1.0939


 INSTANT    0.422000000E-02   TIME STEP NUMBER             422
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925624E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19073E-01 0.46951E+01
   Friction velocity        uk    :  0.19073E-01 0.46911E+01
   Dimensionless distance   yplus :  0.12932E-01 0.29633E+01
   Friction thermal sca.    tstar :  0.52520E+00 0.13996E+03
   Rough dim-less th. sca.  tplus :  0.91609E-02 0.20992E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27575E+00       9   0.44690E-05   0.13089E+01 0.18545E+02 
c  Velocity[X]                                      0.56800E+00 
c  Velocity[Y]                                      0.35681E+00 
c  Velocity[Z]                                      0.38405E+00 
c  Pressure     0.10028E-04      15   0.16918E-03   0.99082E-02 0.82436E+01 
c  k            0.92362E-02      11   0.10554E-04   0.19866E-01 0.48322E+02 
c  omega        0.27922E+07       1   0.57594E-07   0.80153E+07 0.46159E+00 
c  TempK        0.98462E+04       6   0.40347E-05   0.40906E+02 0.23384E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3869e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.283          19.298       0.0060489       -0.011882
v  Velocity[Y]             -15.797          15.566         0.10705         0.14848
v  Velocity[Z]             -26.066          17.895         -1.6646        -0.51225
v  ǁVelocityǁ         0.00095131          26.235          7.7714          6.7699
v  Pressure                -522.49          213.45              36          39.006
v  k                    1.017e-010          6.9495         0.13188         0.25048
v  omega                    57.513     2.7316e+008     1.2912e+006           76861
v  TempK                     298.3          363.17           331.4          335.77
v  TurbVisc            2.5487e-018      0.00058799     3.2082e-005      0.00010943
v  CourantNb            0.00013012          1.5657         0.79747         0.97662
v  FourierNb             0.0036982               1          0.3923         0.11739
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038599      7.314e-005       0.0001949

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.87          306.13
v  Yplus               0          2.9633          0.6353         0.49267


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76168          2.1504          1.1898           1.094


 INSTANT    0.423000000E-02   TIME STEP NUMBER             423
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925632E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19052E-01 0.46948E+01
   Friction velocity        uk    :  0.19052E-01 0.46908E+01
   Dimensionless distance   yplus :  0.12918E-01 0.29632E+01
   Friction thermal sca.    tstar :  0.53432E+00 0.14011E+03
   Rough dim-less th. sca.  tplus :  0.91510E-02 0.20991E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27581E+00       9   0.44774E-05   0.12987E+01 0.18508E+02 
c  Velocity[X]                                      0.56677E+00 
c  Velocity[Y]                                      0.35545E+00 
c  Velocity[Z]                                      0.37646E+00 
c  Pressure     0.93606E-05      16   0.16705E-03   0.92492E-02 0.84865E+01 
c  k            0.92738E-02      11   0.10573E-04   0.19834E-01 0.48120E+02 
c  omega        0.27922E+07       1   0.56449E-07   0.62760E+07 0.41513E+00 
c  TempK        0.98489E+04       6   0.40162E-05   0.40473E+02 0.23273E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3828e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.283          19.299       0.0059973       -0.011879
v  Velocity[Y]             -15.893          15.564         0.10743         0.14898
v  Velocity[Z]             -26.064          17.448         -1.6647         -0.5122
v  ǁVelocityǁ         0.00095171          26.234          7.7716          6.7704
v  Pressure                 -521.9          213.41          35.962          38.964
v  k                    1.017e-010          6.9483         0.13218         0.25134
v  omega                    57.513     2.7316e+008     1.2912e+006           76862
v  TempK                     298.3          363.17          331.43          335.82
v  TurbVisc            2.5485e-018      0.00059206     3.2162e-005      0.00010979
v  CourantNb            0.00013063          1.5667         0.79745         0.97662
v  FourierNb             0.0036985               1         0.39237         0.11755
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037933     7.3136e-005      0.00019489

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.87          306.14
v  Yplus               0          2.9632          0.6353          0.4927


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67316          2.1514          1.1898          1.0942


 INSTANT    0.424000000E-02   TIME STEP NUMBER             424
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925601E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19022E-01 0.46945E+01
   Friction velocity        uk    :  0.19022E-01 0.46905E+01
   Dimensionless distance   yplus :  0.12897E-01 0.29630E+01
   Friction thermal sca.    tstar :  0.54353E+00 0.14033E+03
   Rough dim-less th. sca.  tplus :  0.91365E-02 0.20990E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27587E+00       9   0.44919E-05   0.13053E+01 0.18548E+02 
c  Velocity[X]                                      0.56747E+00 
c  Velocity[Y]                                      0.35819E+00 
c  Velocity[Z]                                      0.37963E+00 
c  Pressure     0.92752E-05      15   0.16670E-03   0.91651E-02 0.81637E+01 
c  k            0.93114E-02      11   0.10565E-04   0.19797E-01 0.47933E+02 
c  omega        0.27922E+07       1   0.62787E-07   0.18870E+08 0.67216E+00 
c  TempK        0.98517E+04       6   0.39983E-05   0.40047E+02 0.23162E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3788e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.283            19.3       0.0059457       -0.011875
v  Velocity[Y]             -15.938          15.561         0.10782         0.14947
v  Velocity[Z]             -26.063          16.558         -1.6648        -0.51215
v  ǁVelocityǁ         0.00095208          26.232          7.7718          6.7708
v  Pressure                -521.31          213.38          35.928          38.925
v  k                   1.0169e-010          6.9477         0.13248          0.2522
v  omega                    57.513     2.7316e+008     1.2912e+006           76862
v  TempK                     298.3          363.17          331.46          335.87
v  TurbVisc            2.5484e-018      0.00059614     3.2242e-005      0.00011015
v  CourantNb             0.0001311          1.5677         0.79744         0.97661
v  FourierNb             0.0036988               1         0.39244         0.11771
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037449     7.3131e-005      0.00019488

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.88          306.14
v  Yplus               0           2.963         0.63531         0.49272


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5245          2.1524          1.1899          1.0943


 INSTANT    0.425000000E-02   TIME STEP NUMBER             425
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925561E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18994E-01 0.46943E+01
   Friction velocity        uk    :  0.18994E-01 0.46903E+01
   Dimensionless distance   yplus :  0.12878E-01 0.29628E+01
   Friction thermal sca.    tstar :  0.55284E+00 0.14054E+03
   Rough dim-less th. sca.  tplus :  0.91232E-02 0.20989E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27592E+00       9   0.45097E-05   0.13098E+01 0.18577E+02 
c  Velocity[X]                                      0.56726E+00 
c  Velocity[Y]                                      0.36160E+00 
c  Velocity[Z]                                      0.38092E+00 
c  Pressure     0.92063E-05      16   0.16743E-03   0.90970E-02 0.89482E+01 
c  k            0.93489E-02      11   0.10561E-04   0.19791E-01 0.47794E+02 
c  omega        0.27922E+07       1   0.57882E-07   0.10191E+08 0.51256E+00 
c  TempK        0.98544E+04       6   0.39809E-05   0.39625E+02 0.23051E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3758e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.283          19.301       0.0058909       -0.011869
v  Velocity[Y]             -15.846          15.558         0.10821         0.14997
v  Velocity[Z]             -26.061          16.613         -1.6649         -0.5121
v  ǁVelocityǁ         0.00095226           26.23           7.772          6.7712
v  Pressure                -520.72          213.34          35.886          38.879
v  k                   1.0168e-010          6.9476         0.13278         0.25306
v  omega                    57.513     2.7316e+008     1.2912e+006           76863
v  TempK                    298.31          363.17          331.49          335.92
v  TurbVisc            2.5482e-018      0.00060022     3.2321e-005       0.0001105
v  CourantNb            0.00013159          1.5684         0.79742         0.97661
v  FourierNb             0.0036992               1         0.39251         0.11787
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037498     7.3127e-005      0.00019488

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.88          306.14
v  Yplus               0          2.9628         0.63531         0.49275


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57195          2.1531          1.1899          1.0945


 INSTANT    0.426000000E-02   TIME STEP NUMBER             426
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925281E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18981E-01 0.46940E+01
   Friction velocity        uk    :  0.18981E-01 0.46900E+01
   Dimensionless distance   yplus :  0.12870E-01 0.29627E+01
   Friction thermal sca.    tstar :  0.56222E+00 0.14063E+03
   Rough dim-less th. sca.  tplus :  0.91169E-02 0.20988E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27598E+00       9   0.45366E-05   0.13119E+01 0.18531E+02 
c  Velocity[X]                                      0.56837E+00 
c  Velocity[Y]                                      0.35792E+00 
c  Velocity[Z]                                      0.38563E+00 
c  Pressure     0.94898E-05      15   0.16647E-03   0.93772E-02 0.72124E+01 
c  k            0.93863E-02      11   0.10602E-04   0.19808E-01 0.47689E+02 
c  omega        0.27922E+07       1   0.55671E-07   0.56136E+07 0.39768E+00 
c  TempK        0.98571E+04       6   0.39641E-05   0.39211E+02 0.22940E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3731e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.283          19.302       0.0058325       -0.011863
v  Velocity[Y]             -15.779          15.554          0.1086         0.15047
v  Velocity[Z]             -26.059          15.336          -1.665        -0.51205
v  ǁVelocityǁ         0.00095242          26.229          7.7721          6.7716
v  Pressure                -520.11          213.32           35.86          38.849
v  k                   1.0167e-010          6.9483         0.13308         0.25391
v  omega                    57.512     2.7316e+008     1.2912e+006           76864
v  TempK                    298.31          363.17          331.53          335.97
v  TurbVisc             2.548e-018      0.00060431     3.2401e-005      0.00011086
v  CourantNb            0.00013216          1.5691         0.79741         0.97661
v  FourierNb             0.0036995               1         0.39258         0.11803
v  total_pressure       1.008e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037545     7.3123e-005      0.00019487

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.88          306.14
v  Yplus               0          2.9627         0.63531         0.49278


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4815          2.1538            1.19          1.0946


 INSTANT    0.427000000E-02   TIME STEP NUMBER             427
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925780E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18969E-01 0.46937E+01
   Friction velocity        uk    :  0.18969E-01 0.46897E+01
   Dimensionless distance   yplus :  0.12861E-01 0.29625E+01
   Friction thermal sca.    tstar :  0.57166E+00 0.14073E+03
   Rough dim-less th. sca.  tplus :  0.91109E-02 0.20987E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27604E+00       9   0.45564E-05   0.13217E+01 0.18609E+02 
c  Velocity[X]                                      0.56993E+00 
c  Velocity[Y]                                      0.36297E+00 
c  Velocity[Z]                                      0.38880E+00 
c  Pressure     0.96693E-05      16   0.17002E-03   0.95546E-02 0.10212E+02 
c  k            0.94236E-02      11   0.10701E-04   0.19881E-01 0.47637E+02 
c  omega        0.27922E+07       1   0.57688E-07   0.90133E+07 0.48460E+00 
c  TempK        0.98598E+04       6   0.39478E-05   0.38803E+02 0.22830E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3703e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.283          19.302       0.0057752       -0.011856
v  Velocity[Y]             -15.767          15.549         0.10899         0.15098
v  Velocity[Z]             -26.057          16.454         -1.6651          -0.512
v  ǁVelocityǁ         0.00095283          26.226          7.7723          6.7719
v  Pressure                -519.51          213.26           35.81          38.794
v  k                   1.0166e-010          6.9498         0.13338         0.25475
v  omega                    57.512     2.7316e+008     1.2912e+006           76864
v  TempK                    298.31          363.17          331.56          336.01
v  TurbVisc            2.5478e-018      0.00060841      3.248e-005      0.00011121
v  CourantNb            0.00013264          1.5698         0.79739         0.97661
v  FourierNb             0.0036999               1         0.39266         0.11819
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037589     7.3119e-005      0.00019486

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.89          306.14
v  Yplus               0          2.9625         0.63532          0.4928


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.84941          2.1545            1.19          1.0948


 INSTANT    0.428000000E-02   TIME STEP NUMBER             428
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925494E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18940E-01 0.46934E+01
   Friction velocity        uk    :  0.18940E-01 0.46894E+01
   Dimensionless distance   yplus :  0.12842E-01 0.29623E+01
   Friction thermal sca.    tstar :  0.58117E+00 0.14094E+03
   Rough dim-less th. sca.  tplus :  0.90971E-02 0.20985E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27610E+00       9   0.45730E-05   0.13280E+01 0.18632E+02 
c  Velocity[X]                                      0.57072E+00 
c  Velocity[Y]                                      0.36234E+00 
c  Velocity[Z]                                      0.39494E+00 
c  Pressure     0.10097E-04      16   0.17101E-03   0.99773E-02 0.94701E+01 
c  k            0.94608E-02      11   0.10749E-04   0.19858E-01 0.47430E+02 
c  omega        0.27922E+07       1   0.59489E-07   0.10865E+08 0.52352E+00 
c  TempK        0.98624E+04       6   0.39321E-05   0.38401E+02 0.22719E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3675e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.284          19.302       0.0057141       -0.011847
v  Velocity[Y]             -15.859          15.543         0.10938         0.15148
v  Velocity[Z]             -26.055           15.78         -1.6651        -0.51195
v  ǁVelocityǁ         0.00094453          26.224          7.7724          6.7723
v  Pressure                -518.89          213.22          35.767          38.747
v  k                   1.0165e-010           6.952         0.13368          0.2556
v  omega                    57.512     2.7316e+008     1.2912e+006           76865
v  TempK                    298.31          363.17          331.59          336.06
v  TurbVisc            2.5476e-018      0.00061251     3.2559e-005      0.00011156
v  CourantNb            0.00013272          1.5705         0.79738          0.9766
v  FourierNb             0.0037003               1         0.39273         0.11835
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.003763     7.3115e-005      0.00019486

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.89          306.15
v  Yplus               0          2.9623         0.63532         0.49283


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.32339          2.1551          1.1901           1.095


 INSTANT    0.429000000E-02   TIME STEP NUMBER             429
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925430E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18910E-01 0.46931E+01
   Friction velocity        uk    :  0.18910E-01 0.46891E+01
   Dimensionless distance   yplus :  0.12822E-01 0.29621E+01
   Friction thermal sca.    tstar :  0.59071E+00 0.14116E+03
   Rough dim-less th. sca.  tplus :  0.90828E-02 0.20983E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27616E+00       9   0.45879E-05   0.13361E+01 0.18648E+02 
c  Velocity[X]                                      0.57240E+00 
c  Velocity[Y]                                      0.36320E+00 
c  Velocity[Z]                                      0.40045E+00 
c  Pressure     0.97095E-05      16   0.16949E-03   0.95943E-02 0.95830E+01 
c  k            0.94980E-02      11   0.10787E-04   0.19806E-01 0.47244E+02 
c  omega        0.27922E+07       1   0.63748E-07   0.21003E+08 0.70692E+00 
c  TempK        0.98651E+04       6   0.39167E-05   0.38005E+02 0.22608E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3649e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.284          19.303       0.0056561       -0.011837
v  Velocity[Y]             -15.898          15.537         0.10977         0.15199
v  Velocity[Z]             -26.052          15.654         -1.6652         -0.5119
v  ǁVelocityǁ         0.00093198          26.221          7.7726          6.7727
v  Pressure                -518.28          213.18          35.721          38.697
v  k                   1.0165e-010          7.2378         0.13398         0.25644
v  omega                    57.511     2.7316e+008     1.2912e+006           76866
v  TempK                    298.32          363.17          331.62          336.11
v  TurbVisc            2.5473e-018      0.00061662     3.2637e-005       0.0001119
v  CourantNb            0.00012882          1.5711         0.79736          0.9766
v  FourierNb             0.0037006               1          0.3928         0.11851
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037666     7.3111e-005      0.00019485

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.89          306.15
v  Yplus               0          2.9621         0.63532         0.49286


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85711          2.1558          1.1902          1.0951


 INSTANT    0.430000000E-02   TIME STEP NUMBER             430
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925545E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18882E-01 0.46928E+01
   Friction velocity        uk    :  0.18882E-01 0.46888E+01
   Dimensionless distance   yplus :  0.12802E-01 0.29619E+01
   Friction thermal sca.    tstar :  0.60030E+00 0.14137E+03
   Rough dim-less th. sca.  tplus :  0.90690E-02 0.20982E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27621E+00       9   0.46037E-05   0.13326E+01 0.18670E+02 
c  Velocity[X]                                      0.57270E+00 
c  Velocity[Y]                                      0.36718E+00 
c  Velocity[Z]                                      0.39268E+00 
c  Pressure     0.94111E-05      16   0.16801E-03   0.92996E-02 0.10868E+02 
c  k            0.95350E-02      11   0.10889E-04   0.19837E-01 0.47125E+02 
c  omega        0.27922E+07       1   0.58229E-07   0.11202E+08 0.53553E+00 
c  TempK        0.98677E+04       6   0.39018E-05   0.37615E+02 0.22497E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3633e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.284          19.303       0.0055955       -0.011825
v  Velocity[Y]             -15.799           15.53         0.11017          0.1525
v  Velocity[Z]              -26.05          14.728         -1.6653        -0.51185
v  ǁVelocityǁ         0.00091864          26.219          7.7727           6.773
v  Pressure                -517.69          213.12          35.664          38.637
v  k                   1.0164e-010          8.1328         0.13428         0.25727
v  omega                    57.511     2.7316e+008     1.2912e+006           76866
v  TempK                    298.32          363.17          331.66          336.16
v  TurbVisc            2.5471e-018      0.00062064     3.2715e-005      0.00011225
v  CourantNb            7.151e-005          1.5715         0.79734          0.9766
v  FourierNb              0.003701               1         0.39287         0.11866
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037698     7.3107e-005      0.00019485

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           304.9          306.15
v  Yplus               0          2.9619         0.63533         0.49289


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66841          2.1562          1.1902          1.0953


 INSTANT    0.431000000E-02   TIME STEP NUMBER             431
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925289E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18866E-01 0.46925E+01
   Friction velocity        uk    :  0.18866E-01 0.46885E+01
   Dimensionless distance   yplus :  0.12791E-01 0.29617E+01
   Friction thermal sca.    tstar :  0.60992E+00 0.14149E+03
   Rough dim-less th. sca.  tplus :  0.90613E-02 0.20981E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27627E+00       9   0.46268E-05   0.13324E+01 0.18608E+02 
c  Velocity[X]                                      0.57448E+00 
c  Velocity[Y]                                      0.36335E+00 
c  Velocity[Z]                                      0.39461E+00 
c  Pressure     0.96555E-05      16   0.17021E-03   0.95413E-02 0.10058E+02 
c  k            0.95720E-02      11   0.10986E-04   0.19967E-01 0.47173E+02 
c  omega        0.27922E+07       1   0.53956E-07   0.36441E+07 0.34602E+00 
c  TempK        0.98703E+04       6   0.38872E-05   0.37232E+02 0.22386E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.362e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.284          19.303       0.0055354       -0.011812
v  Velocity[Y]             -15.723          15.523         0.11056         0.15301
v  Velocity[Z]             -26.047          15.254         -1.6653         -0.5118
v  ǁVelocityǁ         0.00090646          26.216          7.7729          6.7734
v  Pressure                -517.11          213.07          35.614          38.583
v  k                   1.0163e-010          9.0201         0.13458         0.25811
v  omega                    57.511     2.7316e+008     1.2912e+006           76867
v  TempK                    298.32          363.17          331.69          336.21
v  TurbVisc            2.5468e-018      0.00062252     3.2793e-005      0.00011259
v  CourantNb           6.9707e-005          1.5718         0.79732         0.97659
v  FourierNb             0.0037015               1         0.39294         0.11882
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037724     7.3103e-005      0.00019484

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           304.9          306.15
v  Yplus               0          2.9617         0.63533         0.49291


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50826          2.1565          1.1903          1.0954


 INSTANT    0.432000000E-02   TIME STEP NUMBER             432
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925168E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18848E-01 0.46922E+01
   Friction velocity        uk    :  0.18848E-01 0.46882E+01
   Dimensionless distance   yplus :  0.12779E-01 0.29614E+01
   Friction thermal sca.    tstar :  0.61956E+00 0.14163E+03
   Rough dim-less th. sca.  tplus :  0.90527E-02 0.20979E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27632E+00       9   0.46521E-05   0.13400E+01 0.18655E+02 
c  Velocity[X]                                      0.57756E+00 
c  Velocity[Y]                                      0.36508E+00 
c  Velocity[Z]                                      0.39735E+00 
c  Pressure     0.10058E-04      16   0.16947E-03   0.99388E-02 0.97414E+01 
c  k            0.96089E-02      11   0.11102E-04   0.20135E-01 0.47336E+02 
c  omega        0.27922E+07       1   0.55687E-07   0.57482E+07 0.40982E+00 
c  TempK        0.98729E+04       6   0.38731E-05   0.36855E+02 0.22275E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3607e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.285          19.303       0.0054776       -0.011797
v  Velocity[Y]             -15.703          15.514         0.11096         0.15353
v  Velocity[Z]             -26.044          14.174         -1.6654        -0.51174
v  ǁVelocityǁ         0.00089277          26.214           7.773          6.7737
v  Pressure                -516.53          213.02          35.567          38.532
v  k                   1.0162e-010          9.9503         0.13488         0.25894
v  omega                    57.511     2.7316e+008     1.2912e+006           76867
v  TempK                    298.32          363.17          331.72          336.26
v  TurbVisc            2.5466e-018      0.00062446     3.2871e-005      0.00011293
v  CourantNb             0.0001315          1.5722         0.79731         0.97659
v  FourierNb             0.0037019               1         0.39301         0.11897
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037746     7.3099e-005      0.00019483

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.91          306.15
v  Yplus               0          2.9614         0.63533         0.49294


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81483          2.1568          1.1903          1.0956


 INSTANT    0.433000000E-02   TIME STEP NUMBER             433
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925268E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18822E-01 0.46920E+01
   Friction velocity        uk    :  0.18822E-01 0.46880E+01
   Dimensionless distance   yplus :  0.12761E-01 0.29612E+01
   Friction thermal sca.    tstar :  0.62920E+00 0.14182E+03
   Rough dim-less th. sca.  tplus :  0.90402E-02 0.20977E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27638E+00       9   0.46680E-05   0.13516E+01 0.18768E+02 
c  Velocity[X]                                      0.58024E+00 
c  Velocity[Y]                                      0.37074E+00 
c  Velocity[Z]                                      0.40058E+00 
c  Pressure     0.10017E-04      16   0.16887E-03   0.98982E-02 0.99108E+01 
c  k            0.96457E-02      11   0.11083E-04   0.19856E-01 0.46794E+02 
c  omega        0.27922E+07       1   0.59900E-07   0.11813E+08 0.54662E+00 
c  TempK        0.98755E+04       6   0.38594E-05   0.36485E+02 0.22164E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3593e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.285          19.303       0.0054214       -0.011782
v  Velocity[Y]              -15.79          15.506         0.11135         0.15404
v  Velocity[Z]             -26.041          15.074         -1.6655        -0.51169
v  ǁVelocityǁ         0.00088092           26.21          7.7732           6.774
v  Pressure                -515.96          212.98          35.521          38.482
v  k                    1.016e-010          10.682         0.13518         0.25976
v  omega                     57.51     2.7316e+008     1.2912e+006           76868
v  TempK                    298.33          363.17          331.75           336.3
v  TurbVisc            2.5463e-018      0.00062701     3.2948e-005      0.00011327
v  CourantNb            0.00013211          1.5725         0.79729         0.97659
v  FourierNb             0.0037023               1         0.39309         0.11912
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037763     7.3095e-005      0.00019483

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.91          306.16
v  Yplus               0          2.9612         0.63534         0.49296


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49114          2.1571          1.1904          1.0957


 INSTANT    0.434000000E-02   TIME STEP NUMBER             434
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925516E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18790E-01 0.46917E+01
   Friction velocity        uk    :  0.18790E-01 0.46877E+01
   Dimensionless distance   yplus :  0.12740E-01 0.29609E+01
   Friction thermal sca.    tstar :  0.63884E+00 0.14206E+03
   Rough dim-less th. sca.  tplus :  0.90250E-02 0.20975E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27644E+00       9   0.46800E-05   0.13572E+01 0.18793E+02 
c  Velocity[X]                                      0.58212E+00 
c  Velocity[Y]                                      0.37242E+00 
c  Velocity[Z]                                      0.40269E+00 
c  Pressure     0.10095E-04      16   0.17081E-03   0.99760E-02 0.12018E+02 
c  k            0.96824E-02      11   0.11102E-04   0.19692E-01 0.46458E+02 
c  omega        0.27922E+07       1   0.67053E-07   0.26190E+08 0.78756E+00 
c  TempK        0.98780E+04       6   0.38460E-05   0.36122E+02 0.22054E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3582e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.285          19.303       0.0053678       -0.011767
v  Velocity[Y]             -15.827          15.496         0.11175         0.15456
v  Velocity[Z]             -26.038          14.324         -1.6655        -0.51163
v  ǁVelocityǁ         0.00083754          26.207          7.7733          6.7743
v  Pressure                -515.43          212.92          35.458          38.415
v  k                   1.0159e-010          10.827         0.13548         0.26059
v  omega                     57.51     2.7316e+008     1.2912e+006           76868
v  TempK                    298.33          363.17          331.78          336.35
v  TurbVisc            2.5461e-018      0.00063112     3.3026e-005       0.0001136
v  CourantNb            0.00013199          1.5728         0.79728         0.97658
v  FourierNb             0.0037028               1         0.39316         0.11927
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037762     7.3092e-005      0.00019482

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.91          306.16
v  Yplus               0          2.9609         0.63534         0.49298


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59747          2.1574          1.1904          1.0959


 INSTANT    0.435000000E-02   TIME STEP NUMBER             435
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925147E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18759E-01 0.46914E+01
   Friction velocity        uk    :  0.18759E-01 0.46874E+01
   Dimensionless distance   yplus :  0.12719E-01 0.29607E+01
   Friction thermal sca.    tstar :  0.64849E+00 0.14229E+03
   Rough dim-less th. sca.  tplus :  0.90104E-02 0.20974E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27649E+00       9   0.46910E-05   0.13637E+01 0.18797E+02 
c  Velocity[X]                                      0.58217E+00 
c  Velocity[Y]                                      0.37460E+00 
c  Velocity[Z]                                      0.40696E+00 
c  Pressure     0.10475E-04      16   0.17410E-03   0.10351E-01 0.10983E+02 
c  k            0.97191E-02      11   0.11086E-04   0.19701E-01 0.46340E+02 
c  omega        0.27922E+07       1   0.59122E-07   0.12622E+08 0.57110E+00 
c  TempK        0.98806E+04       6   0.38328E-05   0.35764E+02 0.21944E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.358e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.285          19.303       0.0053123       -0.011752
v  Velocity[Y]             -15.728          15.486         0.11216         0.15508
v  Velocity[Z]             -26.035          14.492         -1.6655        -0.51158
v  ǁVelocityǁ         0.00085604          26.204          7.7734          6.7747
v  Pressure                 -514.9          212.86          35.402          38.356
v  k                   1.0158e-010          10.684         0.13578         0.26141
v  omega                     57.51     2.7316e+008     1.2912e+006           76869
v  TempK                    298.33          363.17          331.82           336.4
v  TurbVisc            2.5458e-018      0.00063523     3.3102e-005      0.00011394
v  CourantNb            0.00013188          1.5728         0.79726         0.97658
v  FourierNb             0.0037032               1         0.39323         0.11943
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037786      7.309e-005      0.00019482

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.92          306.16
v  Yplus               0          2.9607         0.63534         0.49301


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.32138          2.1575          1.1905           1.096


 INSTANT    0.436000000E-02   TIME STEP NUMBER             436
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925392E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18744E-01 0.46911E+01
   Friction velocity        uk    :  0.18744E-01 0.46871E+01
   Dimensionless distance   yplus :  0.12709E-01 0.29604E+01
   Friction thermal sca.    tstar :  0.65812E+00 0.14241E+03
   Rough dim-less th. sca.  tplus :  0.90031E-02 0.20972E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27655E+00       9   0.46927E-05   0.13651E+01 0.18739E+02 
c  Velocity[X]                                      0.58245E+00 
c  Velocity[Y]                                      0.37016E+00 
c  Velocity[Z]                                      0.41245E+00 
c  Pressure     0.10080E-04      16   0.17436E-03   0.99605E-02 0.13333E+02 
c  k            0.97557E-02      11   0.11143E-04   0.19766E-01 0.46338E+02 
c  omega        0.27922E+07       1   0.54028E-07   0.37940E+07 0.36015E+00 
c  TempK        0.98831E+04       6   0.38200E-05   0.35412E+02 0.21834E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3582e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.285          19.303       0.0052603       -0.011737
v  Velocity[Y]             -15.649          15.475         0.11256          0.1556
v  Velocity[Z]             -26.031          13.375         -1.6656        -0.51153
v  ǁVelocityǁ         0.00084315          26.201          7.7735          6.7749
v  Pressure                -514.39          212.79          35.329           38.28
v  k                   1.0157e-010          10.383         0.13607         0.26223
v  omega                     57.51     2.7316e+008     1.2912e+006           76870
v  TempK                    298.33          363.17          331.85          336.45
v  TurbVisc            2.5455e-018      0.00063932     3.3179e-005      0.00011427
v  CourantNb            0.00013176          1.5728         0.79724         0.97658
v  FourierNb             0.0037037               1          0.3933         0.11958
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037861     7.3086e-005      0.00019481

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.92          306.16
v  Yplus               0          2.9604         0.63533         0.49303


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7549          2.1574          1.1905          1.0962


 INSTANT    0.437000000E-02   TIME STEP NUMBER             437
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925100E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18723E-01 0.46908E+01
   Friction velocity        uk    :  0.18723E-01 0.46868E+01
   Dimensionless distance   yplus :  0.12695E-01 0.29602E+01
   Friction thermal sca.    tstar :  0.66773E+00 0.14257E+03
   Rough dim-less th. sca.  tplus :  0.89929E-02 0.20970E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27660E+00       9   0.46995E-05   0.13582E+01 0.18738E+02 
c  Velocity[X]                                      0.58281E+00 
c  Velocity[Y]                                      0.37097E+00 
c  Velocity[Z]                                      0.40442E+00 
c  Pressure     0.98048E-05      16   0.17486E-03   0.96888E-02 0.10616E+02 
c  k            0.97921E-02      11   0.11202E-04   0.19792E-01 0.46273E+02 
c  omega        0.27922E+07       1   0.53615E-07   0.33284E+07 0.34787E+00 
c  TempK        0.98856E+04       6   0.38075E-05   0.35067E+02 0.21725E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3582e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.285          19.303       0.0052092       -0.011723
v  Velocity[Y]             -15.623          15.464         0.11297         0.15613
v  Velocity[Z]             -26.028           14.24         -1.6656        -0.51147
v  ǁVelocityǁ         0.00083141          26.197          7.7737          6.7752
v  Pressure                -513.88          212.74          35.275          38.224
v  k                   1.0156e-010          10.065         0.13637         0.26304
v  omega                     57.51     2.7316e+008     1.2912e+006           76870
v  TempK                    298.34          363.17          331.88          336.49
v  TurbVisc            2.5452e-018      0.00064341     3.3256e-005       0.0001146
v  CourantNb            0.00013165          1.5728         0.79723         0.97657
v  FourierNb             0.0037042               1         0.39337         0.11973
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038441     7.3085e-005      0.00019481

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.92          306.16
v  Yplus               0          2.9602         0.63533         0.49305


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71644          2.1574          1.1906          1.0963


 INSTANT    0.438000000E-02   TIME STEP NUMBER             438
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925335E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18699E-01 0.46905E+01
   Friction velocity        uk    :  0.18699E-01 0.46865E+01
   Dimensionless distance   yplus :  0.12678E-01 0.29599E+01
   Friction thermal sca.    tstar :  0.67731E+00 0.14275E+03
   Rough dim-less th. sca.  tplus :  0.89815E-02 0.20968E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27665E+00       9   0.47094E-05   0.13656E+01 0.18818E+02 
c  Velocity[X]                                      0.58343E+00 
c  Velocity[Y]                                      0.37199E+00 
c  Velocity[Z]                                      0.41021E+00 
c  Pressure     0.98336E-05      16   0.17275E-03   0.97168E-02 0.12195E+02 
c  k            0.98286E-02      11   0.11280E-04   0.19787E-01 0.46103E+02 
c  omega        0.27922E+07       1   0.57164E-07   0.78581E+07 0.46567E+00 
c  TempK        0.98881E+04       6   0.37952E-05   0.34724E+02 0.21615E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3581e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.285          19.303       0.0051581       -0.011709
v  Velocity[Y]             -15.683          15.453         0.11338         0.15665
v  Velocity[Z]             -26.024          13.671         -1.6656        -0.51142
v  ǁVelocityǁ          0.0008186          26.194          7.7738          6.7755
v  Pressure                -513.36          212.68          35.211          38.156
v  k                   1.0155e-010          9.6004         0.13666         0.26385
v  omega                    57.509     2.7315e+008     1.2912e+006           76871
v  TempK                    298.34          363.17          331.91          336.54
v  TurbVisc            2.5449e-018      0.00064749     3.3332e-005      0.00011493
v  CourantNb            0.00013154          1.5728         0.79721         0.97657
v  FourierNb             0.0037047               1         0.39345         0.11988
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006         0.00381     7.3083e-005      0.00019481

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.93          306.17
v  Yplus               0          2.9599         0.63534         0.49307


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45073          2.1574          1.1907          1.0965


 INSTANT    0.439000000E-02   TIME STEP NUMBER             439
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925249E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18667E-01 0.46902E+01
   Friction velocity        uk    :  0.18667E-01 0.46862E+01
   Dimensionless distance   yplus :  0.12657E-01 0.29597E+01
   Friction thermal sca.    tstar :  0.68685E+00 0.14300E+03
   Rough dim-less th. sca.  tplus :  0.89661E-02 0.20966E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27671E+00       9   0.47191E-05   0.13742E+01 0.18941E+02 
c  Velocity[X]                                      0.58414E+00 
c  Velocity[Y]                                      0.37891E+00 
c  Velocity[Z]                                      0.41113E+00 
c  Pressure     0.97725E-05      16   0.16968E-03   0.96561E-02 0.10851E+02 
c  k            0.98649E-02      11   0.11422E-04   0.19931E-01 0.46148E+02 
c  omega        0.27922E+07       1   0.63756E-07   0.20348E+08 0.70151E+00 
c  TempK        0.98906E+04       6   0.37832E-05   0.34383E+02 0.21504E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3581e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.286          19.303         0.00511       -0.011695
v  Velocity[Y]             -15.722          15.441         0.11379         0.15718
v  Velocity[Z]              -26.02          13.575         -1.6657        -0.51137
v  ǁVelocityǁ         0.00080687           26.19          7.7739          6.7758
v  Pressure                -512.83          212.63          35.159            38.1
v  k                   1.0153e-010          8.7389         0.13696         0.26466
v  omega                    57.509     2.7315e+008     1.2912e+006           76871
v  TempK                    298.34          363.17          331.94          336.59
v  TurbVisc            2.5446e-018      0.00065156     3.3408e-005      0.00011526
v  CourantNb            0.00013143          1.5728         0.79719         0.97657
v  FourierNb             0.0037052               1         0.39352         0.12003
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038108      7.308e-005      0.00019481

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.93          306.17
v  Yplus               0          2.9597         0.63534         0.49309


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61759          2.1574          1.1907          1.0966


 INSTANT    0.440000000E-02   TIME STEP NUMBER             440
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925472E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18638E-01 0.46899E+01
   Friction velocity        uk    :  0.18638E-01 0.46859E+01
   Dimensionless distance   yplus :  0.12637E-01 0.29593E+01
   Friction thermal sca.    tstar :  0.69634E+00 0.14322E+03
   Rough dim-less th. sca.  tplus :  0.89519E-02 0.20964E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27676E+00       9   0.47303E-05   0.13769E+01 0.18942E+02 
c  Velocity[X]                                      0.58388E+00 
c  Velocity[Y]                                      0.38067E+00 
c  Velocity[Z]                                      0.41230E+00 
c  Pressure     0.97975E-05      16   0.17177E-03   0.96803E-02 0.14939E+02 
c  k            0.99012E-02      11   0.11420E-04   0.19877E-01 0.45945E+02 
c  omega        0.27922E+07       1   0.62369E-07   0.16884E+08 0.64861E+00 
c  TempK        0.98930E+04       6   0.37714E-05   0.34045E+02 0.21392E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3589e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.286          19.303       0.0050568       -0.011683
v  Velocity[Y]             -15.634          15.429         0.11421         0.15771
v  Velocity[Z]             -26.016          12.846         -1.6657        -0.51131
v  ǁVelocityǁ          0.0007941          26.186           7.774           6.776
v  Pressure                -512.34          212.54          35.074          38.013
v  k                   1.0152e-010          7.7879         0.13725         0.26547
v  omega                    57.509     2.7315e+008     1.2912e+006           76872
v  TempK                    298.34          363.17          331.97          336.63
v  TurbVisc            2.5443e-018      0.00065562     3.3484e-005      0.00011558
v  CourantNb            0.00013132          1.5726         0.79718         0.97657
v  FourierNb             0.0037057               1         0.39359         0.12018
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038173     7.3078e-005       0.0001948

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.93          306.17
v  Yplus               0          2.9593         0.63534         0.49312


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4232          2.1572          1.1908          1.0967


 INSTANT    0.441000000E-02   TIME STEP NUMBER             441
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925107E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18619E-01 0.46897E+01
   Friction velocity        uk    :  0.18619E-01 0.46857E+01
   Dimensionless distance   yplus :  0.12624E-01 0.29591E+01
   Friction thermal sca.    tstar :  0.70580E+00 0.14337E+03
   Rough dim-less th. sca.  tplus :  0.89427E-02 0.20962E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27681E+00       9   0.47399E-05   0.13709E+01 0.18825E+02 
c  Velocity[X]                                      0.58383E+00 
c  Velocity[Y]                                      0.37473E+00 
c  Velocity[Z]                                      0.41233E+00 
c  Pressure     0.98712E-05      16   0.17463E-03   0.97526E-02 0.13397E+02 
c  k            0.99374E-02      11   0.11382E-04   0.19730E-01 0.45639E+02 
c  omega        0.27922E+07       1   0.54528E-07   0.45439E+07 0.38625E+00 
c  TempK        0.98955E+04       6   0.37598E-05   0.33714E+02 0.21280E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3601e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.286          19.303        0.005003       -0.011672
v  Velocity[Y]             -15.545          15.417         0.11463         0.15824
v  Velocity[Z]             -26.012          13.157         -1.6657        -0.51126
v  ǁVelocityǁ         0.00078226          26.182           7.774          6.7763
v  Pressure                -511.84          212.47          35.001          37.938
v  k                   1.0151e-010          7.0665         0.13754         0.26627
v  omega                    57.509     2.7315e+008     1.2912e+006           76872
v  TempK                    298.35          363.17             332          336.68
v  TurbVisc             2.544e-018      0.00065967      3.356e-005       0.0001159
v  CourantNb            0.00013121          1.5723         0.79716         0.97656
v  FourierNb             0.0037062               1         0.39366         0.12033
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038226     7.3077e-005       0.0001948

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.94          306.17
v  Yplus               0          2.9591         0.63533         0.49314


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49214          2.1569          1.1908          1.0969


 INSTANT    0.442000000E-02   TIME STEP NUMBER             442
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925162E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18601E-01 0.46894E+01
   Friction velocity        uk    :  0.18601E-01 0.46854E+01
   Dimensionless distance   yplus :  0.12612E-01 0.29588E+01
   Friction thermal sca.    tstar :  0.71518E+00 0.14351E+03
   Rough dim-less th. sca.  tplus :  0.89343E-02 0.20960E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27686E+00       9   0.47529E-05   0.13694E+01 0.18819E+02 
c  Velocity[X]                                      0.58317E+00 
c  Velocity[Y]                                      0.37510E+00 
c  Velocity[Z]                                      0.41110E+00 
c  Pressure     0.99549E-05      16   0.17874E-03   0.98347E-02 0.13638E+02 
c  k            0.99735E-02      11   0.11386E-04   0.19632E-01 0.45420E+02 
c  omega        0.27922E+07       1   0.53946E-07   0.35583E+07 0.36040E+00 
c  TempK        0.98979E+04       6   0.37484E-05   0.33391E+02 0.21170E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3611e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.285          19.304       0.0049478       -0.011662
v  Velocity[Y]             -15.511          15.405         0.11505         0.15877
v  Velocity[Z]             -26.008          12.206         -1.6657        -0.51121
v  ǁVelocityǁ         0.00077036          26.178          7.7741          6.7765
v  Pressure                -511.34           212.4          34.926           37.86
v  k                   1.0149e-010          7.0814         0.13784         0.26707
v  omega                    57.508     2.7315e+008     1.2912e+006           76873
v  TempK                    298.35          363.17          332.03          336.72
v  TurbVisc            2.5436e-018       0.0006637     3.3636e-005      0.00011623
v  CourantNb            0.00013111          1.5721         0.79714         0.97656
v  FourierNb             0.0037067               1         0.39373         0.12048
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038265     7.3077e-005      0.00019481

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.94          306.17
v  Yplus               0          2.9588         0.63533         0.49316


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44579          2.1566          1.1909           1.097


 INSTANT    0.443000000E-02   TIME STEP NUMBER             443
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925178E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18576E-01 0.46891E+01
   Friction velocity        uk    :  0.18576E-01 0.46851E+01
   Dimensionless distance   yplus :  0.12595E-01 0.29585E+01
   Friction thermal sca.    tstar :  0.72451E+00 0.14370E+03
   Rough dim-less th. sca.  tplus :  0.89220E-02 0.20958E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27691E+00       9   0.47617E-05   0.13698E+01 0.18826E+02 
c  Velocity[X]                                      0.58264E+00 
c  Velocity[Y]                                      0.37505E+00 
c  Velocity[Z]                                      0.41207E+00 
c  Pressure     0.99923E-05      16   0.18579E-03   0.98712E-02 0.13539E+02 
c  k            0.10010E-01      11   0.11391E-04   0.19598E-01 0.45274E+02 
c  omega        0.27922E+07       1   0.54444E-07   0.42421E+07 0.37918E+00 
c  TempK        0.99003E+04       6   0.37371E-05   0.33076E+02 0.21061E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3619e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.285          19.304       0.0048929       -0.011653
v  Velocity[Y]             -15.538          15.393         0.11548         0.15931
v  Velocity[Z]             -26.004           13.05         -1.6657        -0.51116
v  ǁVelocityǁ         0.00075888          26.174          7.7742          6.7767
v  Pressure                -510.84          212.32          34.851          37.783
v  k                   1.0148e-010          7.0969         0.13813         0.26787
v  omega                    57.508     2.7315e+008     1.2912e+006           76873
v  TempK                    298.35          363.17          332.06          336.77
v  TurbVisc            2.5433e-018      0.00066772     3.3711e-005      0.00011655
v  CourantNb            0.00013101          1.5719         0.79713         0.97656
v  FourierNb             0.0037073               1         0.39381         0.12064
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038292     7.3076e-005      0.00019481

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.94          306.17
v  Yplus               0          2.9585         0.63533         0.49317


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76088          2.1564          1.1909          1.0972


 INSTANT    0.444000000E-02   TIME STEP NUMBER             444
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925230E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18547E-01 0.46888E+01
   Friction velocity        uk    :  0.18547E-01 0.46848E+01
   Dimensionless distance   yplus :  0.12575E-01 0.29582E+01
   Friction thermal sca.    tstar :  0.73376E+00 0.14393E+03
   Rough dim-less th. sca.  tplus :  0.89082E-02 0.20956E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27697E+00       9   0.47733E-05   0.13823E+01 0.18927E+02 
c  Velocity[X]                                      0.58334E+00 
c  Velocity[Y]                                      0.37633E+00 
c  Velocity[Z]                                      0.42263E+00 
c  Pressure     0.10540E-04      16   0.18413E-03   0.10412E-01 0.12304E+02 
c  k            0.10046E-01      11   0.11459E-04   0.19704E-01 0.45287E+02 
c  omega        0.27922E+07       1   0.61731E-07   0.13945E+08 0.59146E+00 
c  TempK        0.99027E+04       6   0.37261E-05   0.32764E+02 0.20952E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3626e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.285          19.304       0.0048357       -0.011645
v  Velocity[Y]             -15.671           15.38          0.1159         0.15984
v  Velocity[Z]                 -26          12.612         -1.6657         -0.5111
v  ǁVelocityǁ         0.00074732          26.169          7.7743          6.7769
v  Pressure                -510.33          212.26          34.789          37.717
v  k                   1.0147e-010          7.1129         0.13842         0.26867
v  omega                    57.508     2.7315e+008     1.2912e+006           76874
v  TempK                    298.35          363.17          332.09          336.82
v  TurbVisc            2.5429e-018      0.00067172     3.3786e-005      0.00011686
v  CourantNb             0.0001309          1.5717         0.79711         0.97656
v  FourierNb             0.0037078               1         0.39388         0.12079
v  total_pressure      1.0081e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038306     7.3076e-005      0.00019481

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.95          306.18
v  Yplus               0          2.9582         0.63534         0.49319


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.30287          2.1562           1.191          1.0973


 INSTANT    0.445000000E-02   TIME STEP NUMBER             445
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925439E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18512E-01 0.46886E+01
   Friction velocity        uk    :  0.18512E-01 0.46846E+01
   Dimensionless distance   yplus :  0.12551E-01 0.29579E+01
   Friction thermal sca.    tstar :  0.74293E+00 0.14420E+03
   Rough dim-less th. sca.  tplus :  0.88916E-02 0.20954E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27702E+00       9   0.47790E-05   0.13974E+01 0.19088E+02 
c  Velocity[X]                                      0.58474E+00 
c  Velocity[Y]                                      0.38631E+00 
c  Velocity[Z]                                      0.42637E+00 
c  Pressure     0.10150E-04      16   0.18019E-03   0.10026E-01 0.14903E+02 
c  k            0.10082E-01      11   0.11529E-04   0.19693E-01 0.45189E+02 
c  omega        0.27922E+07       1   0.65471E-07   0.23342E+08 0.75025E+00 
c  TempK        0.99050E+04       6   0.37152E-05   0.32457E+02 0.20843E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3644e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.285          19.304       0.0047784       -0.011638
v  Velocity[Y]              -15.61          15.367         0.11633         0.16038
v  Velocity[Z]             -25.995          12.562         -1.6657        -0.51105
v  ǁVelocityǁ         0.00073473          26.165          7.7744          6.7772
v  Pressure                -509.85          212.18          34.706          37.632
v  k                   1.0145e-010          7.1292         0.13871         0.26946
v  omega                    57.508     2.7315e+008     1.2912e+006           76874
v  TempK                    298.36          363.17          332.12          336.86
v  TurbVisc            2.5426e-018      0.00067569     3.3862e-005      0.00011718
v  CourantNb             0.0001308          1.5712          0.7971         0.97656
v  FourierNb             0.0037084               1         0.39395         0.12094
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038306     7.3074e-005      0.00019481

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.95          306.18
v  Yplus               0          2.9579         0.63533         0.49321


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60402          2.1558           1.191          1.0975


 INSTANT    0.446000000E-02   TIME STEP NUMBER             446
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925154E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18487E-01 0.46883E+01
   Friction velocity        uk    :  0.18487E-01 0.46843E+01
   Dimensionless distance   yplus :  0.12535E-01 0.29576E+01
   Friction thermal sca.    tstar :  0.75203E+00 0.14439E+03
   Rough dim-less th. sca.  tplus :  0.88795E-02 0.20952E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27707E+00       9   0.47765E-05   0.13796E+01 0.18954E+02 
c  Velocity[X]                                      0.58355E+00 
c  Velocity[Y]                                      0.37966E+00 
c  Velocity[Z]                                      0.41643E+00 
c  Pressure     0.97967E-05      16   0.17549E-03   0.96760E-02 0.14660E+02 
c  k            0.10117E-01      11   0.11622E-04   0.19608E-01 0.44962E+02 
c  omega        0.27922E+07       1   0.58569E-07   0.10309E+08 0.52268E+00 
c  TempK        0.99074E+04       6   0.37044E-05   0.32153E+02 0.20735E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3665e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.285          19.305       0.0047189       -0.011632
v  Velocity[Y]             -15.523          15.354         0.11676         0.16092
v  Velocity[Z]              -25.99          12.025         -1.6657          -0.511
v  ǁVelocityǁ         0.00072335           26.16          7.7745          6.7774
v  Pressure                -509.38           212.1          34.625           37.55
v  k                   1.0144e-010          7.1453           0.139         0.27025
v  omega                    57.508     2.7315e+008     1.2912e+006           76875
v  TempK                    298.36          363.17          332.15          336.91
v  TurbVisc            2.5422e-018      0.00067966     3.3936e-005       0.0001175
v  CourantNb             0.0001307          1.5707         0.79708         0.97655
v  FourierNb             0.0037089               1         0.39402         0.12109
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038296     7.3071e-005      0.00019482

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.95          306.18
v  Yplus               0          2.9576         0.63533         0.49322


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62885          2.1553          1.1911          1.0976


 INSTANT    0.447000000E-02   TIME STEP NUMBER             447
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925175E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18473E-01 0.46881E+01
   Friction velocity        uk    :  0.18473E-01 0.46841E+01
   Dimensionless distance   yplus :  0.12525E-01 0.29573E+01
   Friction thermal sca.    tstar :  0.76103E+00 0.14450E+03
   Rough dim-less th. sca.  tplus :  0.88728E-02 0.20949E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27712E+00       9   0.47848E-05   0.13796E+01 0.18928E+02 
c  Velocity[X]                                      0.58391E+00 
c  Velocity[Y]                                      0.37768E+00 
c  Velocity[Z]                                      0.41797E+00 
c  Pressure     0.97902E-05      17   0.17093E-03   0.96688E-02 0.15513E+02 
c  k            0.10153E-01      11   0.11682E-04   0.19560E-01 0.44774E+02 
c  omega        0.27922E+07       1   0.54574E-07   0.47408E+07 0.38817E+00 
c  TempK        0.99097E+04       6   0.36938E-05   0.31855E+02 0.20626E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3686e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.285          19.305       0.0046583       -0.011624
v  Velocity[Y]             -15.486          15.342          0.1172         0.16146
v  Velocity[Z]             -25.985          12.213         -1.6657        -0.51095
v  ǁVelocityǁ         0.00071175          26.155          7.7746          6.7776
v  Pressure                -508.93          212.01          34.537           37.46
v  k                   1.0142e-010           7.161         0.13929         0.27104
v  omega                    57.507     2.7315e+008     1.2912e+006           76875
v  TempK                    298.36          363.17          332.18          336.95
v  TurbVisc            2.5419e-018      0.00068361     3.4011e-005      0.00011781
v  CourantNb             0.0001306          1.5702         0.79706         0.97655
v  FourierNb             0.0037094               1         0.39409         0.12124
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038269      7.307e-005      0.00019482

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.96          306.18
v  Yplus               0          2.9573         0.63532         0.49324


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43761          2.1548          1.1912          1.0978


 INSTANT    0.448000000E-02   TIME STEP NUMBER             448
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925182E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18449E-01 0.46878E+01
   Friction velocity        uk    :  0.18449E-01 0.46838E+01
   Dimensionless distance   yplus :  0.12509E-01 0.29569E+01
   Friction thermal sca.    tstar :  0.76995E+00 0.14469E+03
   Rough dim-less th. sca.  tplus :  0.88612E-02 0.20947E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27716E+00       9   0.48005E-05   0.13813E+01 0.18940E+02 
c  Velocity[X]                                      0.58514E+00 
c  Velocity[Y]                                      0.37807E+00 
c  Velocity[Z]                                      0.41814E+00 
c  Pressure     0.99038E-05      16   0.17062E-03   0.97802E-02 0.15408E+02 
c  k            0.10189E-01      11   0.11803E-04   0.19543E-01 0.44631E+02 
c  omega        0.27922E+07       1   0.54047E-07   0.36238E+07 0.35963E+00 
c  TempK        0.99120E+04       6   0.36833E-05   0.31563E+02 0.20519E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3704e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.284          19.305       0.0045973       -0.011617
v  Velocity[Y]             -15.508           15.33         0.11763         0.16201
v  Velocity[Z]             -25.981           12.03         -1.6657         -0.5109
v  ǁVelocityǁ         0.00069993          26.151          7.7747          6.7778
v  Pressure                -508.49          211.93           34.45          37.372
v  k                   1.0141e-010           7.176         0.13959         0.27183
v  omega                    57.507     2.7315e+008     1.2912e+006           76875
v  TempK                    298.36          363.17          332.21             337
v  TurbVisc            2.5415e-018      0.00068756     3.4086e-005      0.00011812
v  CourantNb             0.0001305          1.5698         0.79705         0.97655
v  FourierNb               0.00371               1         0.39416         0.12139
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038228     7.3068e-005      0.00019482

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.96          306.18
v  Yplus               0          2.9569         0.63532         0.49325


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.79486          2.1543          1.1912          1.0979


 INSTANT    0.449000000E-02   TIME STEP NUMBER             449
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925160E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18421E-01 0.46876E+01
   Friction velocity        uk    :  0.18421E-01 0.46836E+01
   Dimensionless distance   yplus :  0.12490E-01 0.29566E+01
   Friction thermal sca.    tstar :  0.77876E+00 0.14491E+03
   Rough dim-less th. sca.  tplus :  0.88477E-02 0.20945E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27721E+00       9   0.48141E-05   0.13886E+01 0.18999E+02 
c  Velocity[X]                                      0.58647E+00 
c  Velocity[Y]                                      0.37886E+00 
c  Velocity[Z]                                      0.42325E+00 
c  Pressure     0.99434E-05      16   0.17088E-03   0.98181E-02 0.14223E+02 
c  k            0.10225E-01      11   0.11909E-04   0.19585E-01 0.44565E+02 
c  omega        0.27922E+07       1   0.60865E-07   0.11830E+08 0.55201E+00 
c  TempK        0.99143E+04       6   0.36729E-05   0.31274E+02 0.20412E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3721e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.284          19.306       0.0045342        -0.01161
v  Velocity[Y]             -15.666          15.317         0.11806         0.16255
v  Velocity[Z]             -25.976          12.132         -1.6657        -0.51085
v  ǁVelocityǁ         0.00068861          26.146          7.7748          6.7779
v  Pressure                -508.04          211.85          34.374          37.293
v  k                   1.0139e-010            7.19         0.13988         0.27261
v  omega                    57.507     2.7315e+008     1.2912e+006           76876
v  TempK                    298.37          363.17          332.24          337.04
v  TurbVisc            2.5411e-018       0.0006915      3.416e-005      0.00011843
v  CourantNb            0.00013065          1.5693         0.79703         0.97655
v  FourierNb             0.0037106               1         0.39424         0.12154
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038164     7.3066e-005      0.00019483

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.96          306.18
v  Yplus               0          2.9566         0.63532         0.49326


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44099          2.1539          1.1913          1.0981


 INSTANT    0.450000000E-02   TIME STEP NUMBER             450
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925256E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18385E-01 0.46873E+01
   Friction velocity        uk    :  0.18385E-01 0.46833E+01
   Dimensionless distance   yplus :  0.12465E-01 0.29564E+01
   Friction thermal sca.    tstar :  0.78747E+00 0.14520E+03
   Rough dim-less th. sca.  tplus :  0.88306E-02 0.20943E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27726E+00       9   0.48258E-05   0.13991E+01 0.19114E+02 
c  Velocity[X]                                      0.58884E+00 
c  Velocity[Y]                                      0.38515E+00 
c  Velocity[Z]                                      0.42516E+00 
c  Pressure     0.10006E-04      16   0.16967E-03   0.98783E-02 0.14736E+02 
c  k            0.10260E-01      11   0.12003E-04   0.19611E-01 0.44486E+02 
c  omega        0.27922E+07       1   0.61095E-07   0.13202E+08 0.58408E+00 
c  TempK        0.99166E+04       6   0.36626E-05   0.30990E+02 0.20305E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3745e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.284          19.306       0.0044716       -0.011602
v  Velocity[Y]             -15.627          15.304         0.11849         0.16309
v  Velocity[Z]             -25.971          12.036         -1.6656         -0.5108
v  ǁVelocityǁ         0.00067654          26.141          7.7749          6.7781
v  Pressure                 -507.6          211.78          34.293          37.211
v  k                   1.0138e-010           7.203         0.14017          0.2734
v  omega                    57.507     2.7315e+008     1.2912e+006           76876
v  TempK                    298.37          363.17          332.27          337.09
v  TurbVisc            2.5407e-018      0.00069544     3.4235e-005      0.00011874
v  CourantNb            0.00013104          1.5688         0.79701         0.97655
v  FourierNb             0.0037112               1         0.39431         0.12168
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038078     7.3063e-005      0.00019483

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.97          306.19
v  Yplus               0          2.9564         0.63532         0.49327


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58009          2.1533          1.1913          1.0982


 INSTANT    0.451000000E-02   TIME STEP NUMBER             451
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925204E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18362E-01 0.46871E+01
   Friction velocity        uk    :  0.18362E-01 0.46831E+01
   Dimensionless distance   yplus :  0.12449E-01 0.29560E+01
   Friction thermal sca.    tstar :  0.79608E+00 0.14538E+03
   Rough dim-less th. sca.  tplus :  0.88193E-02 0.20941E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27731E+00       9   0.48368E-05   0.14033E+01 0.19126E+02 
c  Velocity[X]                                      0.59131E+00 
c  Velocity[Y]                                      0.38609E+00 
c  Velocity[Z]                                      0.42594E+00 
c  Pressure     0.10262E-04      17   0.17218E-03   0.10130E-01 0.15421E+02 
c  k            0.10296E-01      11   0.12069E-04   0.19622E-01 0.44391E+02 
c  omega        0.27922E+07       1   0.63832E-07   0.19386E+08 0.69774E+00 
c  TempK        0.99189E+04       6   0.36524E-05   0.30711E+02 0.20199E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3775e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.283          19.307       0.0044105       -0.011595
v  Velocity[Y]             -15.548          15.292         0.11893         0.16364
v  Velocity[Z]             -25.966          12.039         -1.6656        -0.51076
v  ǁVelocityǁ         0.00066462          26.136           7.775          6.7783
v  Pressure                -507.19          211.69          34.208          37.125
v  k                   1.0136e-010          7.2148         0.14046         0.27418
v  omega                    57.506     2.7315e+008     1.2912e+006           76877
v  TempK                    298.37          363.17          332.29          337.13
v  TurbVisc            2.5403e-018      0.00069938     3.4309e-005      0.00011905
v  CourantNb            0.00013148           1.568           0.797         0.97655
v  FourierNb             0.0037117               1         0.39438         0.12183
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037973     7.3061e-005      0.00019483

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.97          306.19
v  Yplus               0           2.956         0.63532         0.49328


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38846          2.1526          1.1914          1.0984


 INSTANT    0.452000000E-02   TIME STEP NUMBER             452
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925184E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18346E-01 0.46869E+01
   Friction velocity        uk    :  0.18346E-01 0.46829E+01
   Dimensionless distance   yplus :  0.12439E-01 0.29556E+01
   Friction thermal sca.    tstar :  0.80459E+00 0.14551E+03
   Rough dim-less th. sca.  tplus :  0.88118E-02 0.20938E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27736E+00       9   0.48479E-05   0.14006E+01 0.19068E+02 
c  Velocity[X]                                      0.59080E+00 
c  Velocity[Y]                                      0.38317E+00 
c  Velocity[Z]                                      0.42663E+00 
c  Pressure     0.10492E-04      17   0.18183E-03   0.10356E-01 0.16755E+02 
c  k            0.10332E-01      11   0.12155E-04   0.19628E-01 0.44285E+02 
c  omega        0.27922E+07       1   0.56726E-07   0.59547E+07 0.43661E+00 
c  TempK        0.99212E+04       6   0.36424E-05   0.30436E+02 0.20094E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3805e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.283          19.307       0.0043482       -0.011587
v  Velocity[Y]             -15.519          15.281         0.11936         0.16418
v  Velocity[Z]             -25.961          12.058         -1.6656        -0.51071
v  ǁVelocityǁ         0.00065307          26.131           7.775          6.7785
v  Pressure                -506.79           211.6          34.113          37.028
v  k                   1.0135e-010          7.2253         0.14075         0.27496
v  omega                    57.506     2.7315e+008     1.2912e+006           76877
v  TempK                    298.37          363.17          332.32          337.18
v  TurbVisc              2.54e-018      0.00070332     3.4383e-005      0.00011935
v  CourantNb            0.00013191          1.5673         0.79698         0.97655
v  FourierNb             0.0037123               1         0.39445         0.12198
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037827     7.3058e-005      0.00019483

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.97          306.19
v  Yplus               0          2.9556         0.63532         0.49329


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54841          2.1518          1.1914          1.0985


 INSTANT    0.453000000E-02   TIME STEP NUMBER             453
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925179E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18324E-01 0.46867E+01
   Friction velocity        uk    :  0.18323E-01 0.46827E+01
   Dimensionless distance   yplus :  0.12424E-01 0.29553E+01
   Friction thermal sca.    tstar :  0.81298E+00 0.14568E+03
   Rough dim-less th. sca.  tplus :  0.88010E-02 0.20936E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27740E+00       9   0.48541E-05   0.13965E+01 0.19049E+02 
c  Velocity[X]                                      0.59033E+00 
c  Velocity[Y]                                      0.38289E+00 
c  Velocity[Z]                                      0.42327E+00 
c  Pressure     0.10167E-04      16   0.17389E-03   0.10034E-01 0.16781E+02 
c  k            0.10367E-01      11   0.12233E-04   0.19642E-01 0.44191E+02 
c  omega        0.27922E+07       1   0.55768E-07   0.45726E+07 0.40538E+00 
c  TempK        0.99234E+04       6   0.36323E-05   0.30164E+02 0.19990E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3835e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.282          19.308       0.0042845       -0.011578
v  Velocity[Y]             -15.541          15.269         0.11979         0.16473
v  Velocity[Z]             -25.955          12.085         -1.6655        -0.51066
v  ǁVelocityǁ         0.00064095          26.125          7.7751          6.7786
v  Pressure                -506.41          211.51          34.017          36.931
v  k                   1.0133e-010          7.2345         0.14104         0.27573
v  omega                    57.506     2.7315e+008     1.2912e+006           76878
v  TempK                    298.37          363.17          332.35          337.22
v  TurbVisc            2.5396e-018      0.00070727     3.4457e-005      0.00011966
v  CourantNb            0.00013232          1.5665         0.79697         0.97654
v  FourierNb             0.0037129               1         0.39451         0.12213
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037614     7.3056e-005      0.00019484

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.98          306.19
v  Yplus               0          2.9553         0.63531          0.4933


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51682          2.1511          1.1915          1.0987


 INSTANT    0.454000000E-02   TIME STEP NUMBER             454
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925166E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18298E-01 0.46865E+01
   Friction velocity        uk    :  0.18298E-01 0.46825E+01
   Dimensionless distance   yplus :  0.12406E-01 0.29550E+01
   Friction thermal sca.    tstar :  0.82126E+00 0.14589E+03
   Rough dim-less th. sca.  tplus :  0.87886E-02 0.20933E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27745E+00       9   0.48594E-05   0.13983E+01 0.19097E+02 
c  Velocity[X]                                      0.58997E+00 
c  Velocity[Y]                                      0.38341E+00 
c  Velocity[Z]                                      0.42486E+00 
c  Pressure     0.99636E-05      17   0.16648E-03   0.98325E-02 0.15915E+02 
c  k            0.10403E-01      11   0.12268E-04   0.19687E-01 0.44133E+02 
c  omega        0.27922E+07       1   0.62073E-07   0.11828E+08 0.56469E+00 
c  TempK        0.99256E+04       6   0.36224E-05   0.29896E+02 0.19887E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3863e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.282          19.308       0.0042194       -0.011569
v  Velocity[Y]             -15.686          15.257         0.12021         0.16528
v  Velocity[Z]              -25.95          12.111         -1.6655        -0.51062
v  ǁVelocityǁ         0.00062882           26.12          7.7752          6.7788
v  Pressure                -506.02          211.42          33.929          36.841
v  k                   1.0131e-010          7.2423         0.14132         0.27651
v  omega                    57.506     2.7315e+008     1.2912e+006           76878
v  TempK                    298.38          363.17          332.38          337.27
v  TurbVisc            2.5392e-018      0.00071122     3.4531e-005      0.00011996
v  CourantNb            0.00013276          1.5659         0.79695         0.97654
v  FourierNb             0.0037135               1         0.39458         0.12228
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.003733     7.3053e-005      0.00019484

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.98          306.19
v  Yplus               0           2.955         0.63531         0.49331


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62363          2.1504          1.1915          1.0988


 INSTANT    0.455000000E-02   TIME STEP NUMBER             455
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925238E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18266E-01 0.46863E+01
   Friction velocity        uk    :  0.18266E-01 0.46823E+01
   Dimensionless distance   yplus :  0.12385E-01 0.29547E+01
   Friction thermal sca.    tstar :  0.82941E+00 0.14614E+03
   Rough dim-less th. sca.  tplus :  0.87733E-02 0.20931E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27750E+00       9   0.48719E-05   0.14047E+01 0.19165E+02 
c  Velocity[X]                                      0.59006E+00 
c  Velocity[Y]                                      0.38799E+00 
c  Velocity[Z]                                      0.42660E+00 
c  Pressure     0.10108E-04      17   0.16639E-03   0.99741E-02 0.16320E+02 
c  k            0.10438E-01      11   0.12348E-04   0.19737E-01 0.44076E+02 
c  omega        0.27922E+07       1   0.60268E-07   0.10626E+08 0.54718E+00 
c  TempK        0.99279E+04       6   0.36125E-05   0.29632E+02 0.19784E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3896e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.281          19.309       0.0041524       -0.011561
v  Velocity[Y]             -15.686          15.246         0.12064         0.16583
v  Velocity[Z]             -25.945          12.137         -1.6655        -0.51058
v  ǁVelocityǁ         0.00061697          26.115          7.7753          6.7789
v  Pressure                -505.65          211.33          33.837          36.748
v  k                    1.013e-010          7.2488         0.14161         0.27728
v  omega                    57.505     2.7316e+008     1.2912e+006           76878
v  TempK                    298.38          363.17          332.41          337.31
v  TurbVisc            2.5388e-018      0.00071517     3.4605e-005      0.00012027
v  CourantNb             0.0001332           1.565         0.79694         0.97654
v  FourierNb             0.0037141               1         0.39465         0.12242
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036979      7.305e-005      0.00019484

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.98          306.19
v  Yplus               0          2.9547         0.63531         0.49332


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42263          2.1496          1.1916           1.099


 INSTANT    0.456000000E-02   TIME STEP NUMBER             456
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925185E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18242E-01 0.46862E+01
   Friction velocity        uk    :  0.18242E-01 0.46822E+01
   Dimensionless distance   yplus :  0.12368E-01 0.29544E+01
   Friction thermal sca.    tstar :  0.83746E+00 0.14634E+03
   Rough dim-less th. sca.  tplus :  0.87618E-02 0.20929E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27754E+00       9   0.48746E-05   0.14068E+01 0.19171E+02 
c  Velocity[X]                                      0.58993E+00 
c  Velocity[Y]                                      0.38566E+00 
c  Velocity[Z]                                      0.43120E+00 
c  Pressure     0.10045E-04      17   0.16705E-03   0.99104E-02 0.16219E+02 
c  k            0.10474E-01      11   0.12432E-04   0.19798E-01 0.44034E+02 
c  omega        0.27922E+07       1   0.59225E-07   0.77145E+07 0.48915E+00 
c  TempK        0.99301E+04       6   0.36027E-05   0.29372E+02 0.19683E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3936e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.281          19.309       0.0040846       -0.011553
v  Velocity[Y]             -15.643          15.243         0.12107         0.16638
v  Velocity[Z]              -25.94          12.164         -1.6655        -0.51054
v  ǁVelocityǁ         0.00060419           26.11          7.7754          6.7791
v  Pressure                 -505.3          211.25          33.746          36.656
v  k                   1.0128e-010           7.254          0.1419         0.27805
v  omega                    57.505     2.7316e+008     1.2912e+006           76879
v  TempK                    298.38          363.17          332.44          337.36
v  TurbVisc            2.5384e-018      0.00071913     3.4679e-005      0.00012057
v  CourantNb            0.00013363          1.5641         0.79693         0.97654
v  FourierNb             0.0037147               1         0.39472         0.12257
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036573     7.3048e-005      0.00019485

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.98           306.2
v  Yplus               0          2.9544         0.63531         0.49333


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69693          2.1486          1.1916          1.0991


 INSTANT    0.457000000E-02   TIME STEP NUMBER             457
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925199E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18226E-01 0.46860E+01
   Friction velocity        uk    :  0.18226E-01 0.46820E+01
   Dimensionless distance   yplus :  0.12357E-01 0.29540E+01
   Friction thermal sca.    tstar :  0.84539E+00 0.14647E+03
   Rough dim-less th. sca.  tplus :  0.87540E-02 0.20927E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27759E+00       9   0.48816E-05   0.14039E+01 0.19218E+02 
c  Velocity[X]                                      0.59061E+00 
c  Velocity[Y]                                      0.38820E+00 
c  Velocity[Z]                                      0.42504E+00 
c  Pressure     0.10226E-04      17   0.16449E-03   0.10088E-01 0.16631E+02 
c  k            0.10509E-01      11   0.12449E-04   0.19848E-01 0.43980E+02 
c  omega        0.27922E+07       1   0.65815E-07   0.22302E+08 0.75151E+00 
c  TempK        0.99323E+04       6   0.35930E-05   0.29119E+02 0.19583E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3978e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.281           19.31       0.0040174       -0.011545
v  Velocity[Y]             -15.595          15.248         0.12149         0.16693
v  Velocity[Z]             -25.934           12.19         -1.6654         -0.5105
v  ǁVelocityǁ         0.00059307          26.105          7.7754          6.7792
v  Pressure                -504.96          211.16          33.652          36.561
v  k                   1.0126e-010          7.2578         0.14219         0.27882
v  omega                    57.504     2.7316e+008     1.2912e+006           76879
v  TempK                    298.38          363.17          332.46           337.4
v  TurbVisc            2.5379e-018      0.00072309     3.4752e-005      0.00012087
v  CourantNb            0.00013411           1.563         0.79691         0.97654
v  FourierNb             0.0037153               1         0.39479         0.12272
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036124     7.3045e-005      0.00019485

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.99           306.2
v  Yplus               0           2.954         0.63531         0.49333


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63863          2.1476          1.1917          1.0993


 INSTANT    0.458000000E-02   TIME STEP NUMBER             458
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925123E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18208E-01 0.46859E+01
   Friction velocity        uk    :  0.18208E-01 0.46819E+01
   Dimensionless distance   yplus :  0.12345E-01 0.29537E+01
   Friction thermal sca.    tstar :  0.84884E+00 0.14661E+03
   Rough dim-less th. sca.  tplus :  0.87454E-02 0.20924E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27763E+00       9   0.48903E-05   0.14006E+01 0.19177E+02 
c  Velocity[X]                                      0.59052E+00 
c  Velocity[Y]                                      0.38556E+00 
c  Velocity[Z]                                      0.42449E+00 
c  Pressure     0.97805E-05      16   0.16273E-03   0.96473E-02 0.17632E+02 
c  k            0.10544E-01      11   0.12476E-04   0.19899E-01 0.43932E+02 
c  omega        0.27922E+07       1   0.58429E-07   0.74833E+07 0.48661E+00 
c  TempK        0.99345E+04       6   0.35834E-05   0.28871E+02 0.19484E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4019e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.28           19.31       0.0039491       -0.011539
v  Velocity[Y]             -15.601          15.213         0.12192         0.16749
v  Velocity[Z]             -25.928          12.216         -1.6654        -0.51046
v  ǁVelocityǁ         0.00057998          26.099          7.7755          6.7793
v  Pressure                -504.64          211.06          33.551          36.459
v  k                   1.0125e-010          7.2604         0.14248         0.27959
v  omega                    57.504     2.7316e+008     1.2912e+006           76879
v  TempK                    298.38          363.17          332.49          337.44
v  TurbVisc            2.5375e-018      0.00072704     3.4826e-005      0.00012117
v  CourantNb             0.0001345           1.562         0.79689         0.97654
v  FourierNb             0.0037159               1         0.39486         0.12286
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036302     7.3044e-005      0.00019486

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.99           306.2
v  Yplus               0          2.9537          0.6353         0.49334


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6913          2.1466          1.1918          1.0994


 INSTANT    0.459000000E-02   TIME STEP NUMBER             459
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925182E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18188E-01 0.46857E+01
   Friction velocity        uk    :  0.18188E-01 0.46817E+01
   Dimensionless distance   yplus :  0.12332E-01 0.29533E+01
   Friction thermal sca.    tstar :  0.86087E+00 0.14678E+03
   Rough dim-less th. sca.  tplus :  0.87358E-02 0.20922E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27768E+00       9   0.48984E-05   0.14017E+01 0.19193E+02 
c  Velocity[X]                                      0.59102E+00 
c  Velocity[Y]                                      0.38448E+00 
c  Velocity[Z]                                      0.42620E+00 
c  Pressure     0.97509E-05      16   0.16063E-03   0.96174E-02 0.17607E+02 
c  k            0.10580E-01      11   0.12571E-04   0.19946E-01 0.43891E+02 
c  omega        0.27922E+07       1   0.58617E-07   0.73361E+07 0.47815E+00 
c  TempK        0.99366E+04       6   0.35737E-05   0.28627E+02 0.19386E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4059e-007                             9


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.28           19.31       0.0038809       -0.011534
v  Velocity[Y]             -15.708          15.203         0.12234         0.16804
v  Velocity[Z]             -25.923           12.24         -1.6653        -0.51042
v  ǁVelocityǁ         0.00056857          26.094          7.7756          6.7794
v  Pressure                -504.33          210.96           33.45          36.357
v  k                   1.0123e-010          7.2618         0.14277         0.28036
v  omega                    57.504     2.7316e+008     1.2912e+006           76880
v  TempK                    298.39          363.17          332.52          337.49
v  TurbVisc            2.5371e-018      0.00073097     3.4899e-005      0.00012146
v  CourantNb            0.00013499          1.5611         0.79687         0.97653
v  FourierNb             0.0037164               1         0.39493         0.12301
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.003812     7.3043e-005      0.00019486

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          304.99           306.2
v  Yplus               0          2.9533         0.63529         0.49335


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71656          2.1457          1.1918          1.0995


 INSTANT    0.460000000E-02   TIME STEP NUMBER             460
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925195E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18162E-01 0.46856E+01
   Friction velocity        uk    :  0.18162E-01 0.46816E+01
   Dimensionless distance   yplus :  0.12314E-01 0.29530E+01
   Friction thermal sca.    tstar :  0.86843E+00 0.14699E+03
   Rough dim-less th. sca.  tplus :  0.87233E-02 0.20919E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27772E+00       9   0.49114E-05   0.14081E+01 0.19259E+02 
c  Velocity[X]                                      0.59345E+00 
c  Velocity[Y]                                      0.38724E+00 
c  Velocity[Z]                                      0.42743E+00 
c  Pressure     0.99113E-05      17   0.16054E-03   0.97746E-02 0.17270E+02 
c  k            0.10615E-01      11   0.12716E-04   0.19992E-01 0.43851E+02 
c  omega        0.27922E+07       1   0.64527E-07   0.19343E+08 0.70138E+00 
c  TempK        0.99388E+04       6   0.35642E-05   0.28386E+02 0.19290E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step       6.41e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.28           19.31       0.0038139       -0.011531
v  Velocity[Y]             -15.778          15.193         0.12275          0.1686
v  Velocity[Z]             -25.918          12.264         -1.6653        -0.51038
v  ǁVelocityǁ         0.00055644          26.088          7.7756          6.7795
v  Pressure                -504.03          210.86          33.352          36.257
v  k                   1.0121e-010           7.262         0.14306         0.28113
v  omega                    57.503     2.7316e+008     1.2912e+006           76880
v  TempK                    298.39          363.17          332.55          337.53
v  TurbVisc            2.5367e-018      0.00073488     3.4973e-005      0.00012176
v  CourantNb             0.0001354          1.5601         0.79686         0.97653
v  FourierNb              0.003717               1           0.395         0.12316
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0040689     7.3042e-005      0.00019487

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17             305           306.2
v  Yplus               0           2.953         0.63529         0.49335


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81694          2.1447          1.1919          1.0997


 INSTANT    0.461000000E-02   TIME STEP NUMBER             461
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925202E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18139E-01 0.46854E+01
   Friction velocity        uk    :  0.18138E-01 0.46815E+01
   Dimensionless distance   yplus :  0.12298E-01 0.29527E+01
   Friction thermal sca.    tstar :  0.87587E+00 0.14718E+03
   Rough dim-less th. sca.  tplus :  0.87121E-02 0.20917E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27777E+00       9   0.49264E-05   0.14157E+01 0.19327E+02 
c  Velocity[X]                                      0.59593E+00 
c  Velocity[Y]                                      0.39113E+00 
c  Velocity[Z]                                      0.42861E+00 
c  Pressure     0.99536E-05      17   0.16273E-03   0.98151E-02 0.17385E+02 
c  k            0.10650E-01      11   0.12765E-04   0.20047E-01 0.43827E+02 
c  omega        0.27922E+07       1   0.60137E-07   0.11481E+08 0.56467E+00 
c  TempK        0.99409E+04       6   0.35547E-05   0.28149E+02 0.19195E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4148e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.28           19.31       0.0037429       -0.011529
v  Velocity[Y]             -15.719          15.183         0.12317         0.16915
v  Velocity[Z]             -25.912          12.288         -1.6652        -0.51034
v  ǁVelocityǁ         0.00054458          26.083          7.7757          6.7797
v  Pressure                -503.75          210.77          33.252          36.157
v  k                    1.012e-010          7.2613         0.14335         0.28189
v  omega                    57.503     2.7316e+008     1.2912e+006           76881
v  TempK                    298.39          363.17          332.57          337.57
v  TurbVisc            2.5363e-018      0.00073875     3.5046e-005      0.00012206
v  CourantNb            0.00013584          1.5589         0.79684         0.97653
v  FourierNb             0.0037176               1         0.39507          0.1233
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0041744      7.304e-005      0.00019487

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17             305           306.2
v  Yplus               0          2.9527         0.63529         0.49336


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81426          2.1435          1.1919          1.0998


 INSTANT    0.462000000E-02   TIME STEP NUMBER             462
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925158E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18127E-01 0.46853E+01
   Friction velocity        uk    :  0.18127E-01 0.46813E+01
   Dimensionless distance   yplus :  0.12290E-01 0.29524E+01
   Friction thermal sca.    tstar :  0.88319E+00 0.14727E+03
   Rough dim-less th. sca.  tplus :  0.87065E-02 0.20915E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27781E+00       9   0.49409E-05   0.14167E+01 0.19331E+02 
c  Velocity[X]                                      0.59734E+00 
c  Velocity[Y]                                      0.38786E+00 
c  Velocity[Z]                                      0.43146E+00 
c  Pressure     0.99580E-05      17   0.16827E-03   0.98182E-02 0.17368E+02 
c  k            0.10685E-01      11   0.12854E-04   0.20112E-01 0.43802E+02 
c  omega        0.27922E+07       1   0.58547E-07   0.72974E+07 0.46864E+00 
c  TempK        0.99430E+04       6   0.35453E-05   0.27916E+02 0.19100E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4199e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.279           19.31       0.0036715       -0.011529
v  Velocity[Y]             -15.678          15.198         0.12359         0.16971
v  Velocity[Z]             -25.907           12.31         -1.6652        -0.51031
v  ǁVelocityǁ          0.0005323          26.078          7.7758          6.7798
v  Pressure                -503.48          210.67          33.154          36.057
v  k                   1.0118e-010          7.2596         0.14364         0.28265
v  omega                    57.503     2.7316e+008     1.2912e+006           76881
v  TempK                    298.39          363.17           332.6          337.62
v  TurbVisc            2.5359e-018      0.00074257     3.5119e-005      0.00012235
v  CourantNb            0.00013627          1.5577         0.79682         0.97652
v  FourierNb             0.0037182               1         0.39514         0.12345
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0040951     7.3039e-005      0.00019488

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17             305          306.21
v  Yplus               0          2.9524         0.63528         0.49336


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85997          2.1423           1.192             1.1


 INSTANT    0.463000000E-02   TIME STEP NUMBER             463
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925017E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18114E-01 0.46852E+01
   Friction velocity        uk    :  0.18114E-01 0.46812E+01
   Dimensionless distance   yplus :  0.12281E-01 0.29520E+01
   Friction thermal sca.    tstar :  0.89038E+00 0.14738E+03
   Rough dim-less th. sca.  tplus :  0.87003E-02 0.20912E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27785E+00       9   0.49639E-05   0.14274E+01 0.19442E+02 
c  Velocity[X]                                      0.60073E+00 
c  Velocity[Y]                                      0.39370E+00 
c  Velocity[Z]                                      0.43292E+00 
c  Pressure     0.10121E-04      17   0.17826E-03   0.99779E-02 0.16959E+02 
c  k            0.10720E-01      11   0.12939E-04   0.20179E-01 0.43780E+02 
c  omega        0.27922E+07       1   0.63424E-07   0.17756E+08 0.67600E+00 
c  TempK        0.99452E+04       6   0.35359E-05   0.27687E+02 0.19008E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4248e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.279           19.31       0.0036009       -0.011531
v  Velocity[Y]             -15.687          15.204         0.12401         0.17027
v  Velocity[Z]             -25.901          12.332         -1.6651        -0.51027
v  ǁVelocityǁ         0.00052065          26.072          7.7758          6.7799
v  Pressure                -503.23          210.57          33.058          35.961
v  k                   1.0116e-010          7.2571         0.14393         0.28342
v  omega                    57.502     2.7316e+008     1.2912e+006           76881
v  TempK                    298.39          363.17          332.63          337.66
v  TurbVisc            2.5354e-018      0.00074632     3.5192e-005      0.00012265
v  CourantNb            0.00013672          1.5565         0.79681         0.97652
v  FourierNb             0.0037188               1         0.39521          0.1236
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0040001     7.3038e-005      0.00019488

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17             305          306.21
v  Yplus               0           2.952         0.63528         0.49337


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68998          2.1411           1.192          1.1001


 INSTANT    0.464000000E-02   TIME STEP NUMBER             464
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925140E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18099E-01 0.46851E+01
   Friction velocity        uk    :  0.18099E-01 0.46811E+01
   Dimensionless distance   yplus :  0.12271E-01 0.29517E+01
   Friction thermal sca.    tstar :  0.89389E+00 0.14750E+03
   Rough dim-less th. sca.  tplus :  0.86930E-02 0.20910E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27790E+00       9   0.49969E-05   0.14351E+01 0.19473E+02 
c  Velocity[X]                                      0.60450E+00 
c  Velocity[Y]                                      0.39347E+00 
c  Velocity[Z]                                      0.43715E+00 
c  Pressure     0.10266E-04      17   0.17748E-03   0.10119E-01 0.19257E+02 
c  k            0.10756E-01      11   0.13018E-04   0.20255E-01 0.43769E+02 
c  omega        0.27922E+07       1   0.59396E-07   0.89174E+07 0.50299E+00 
c  TempK        0.99473E+04       6   0.35266E-05   0.27462E+02 0.18916E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4297e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.279           19.31       0.0035296       -0.011535
v  Velocity[Y]             -15.793          15.155         0.12442         0.17083
v  Velocity[Z]             -25.895          12.353         -1.6651        -0.51024
v  ǁVelocityǁ         0.00050934          26.066          7.7759            6.78
v  Pressure                -503.01          210.46          32.947          35.849
v  k                   1.0115e-010          7.2538         0.14422         0.28418
v  omega                    57.502     2.7316e+008     1.2912e+006           76882
v  TempK                     298.4          363.17          332.65           337.7
v  TurbVisc             2.535e-018      0.00075002     3.5265e-005      0.00012294
v  CourantNb            0.00013713          1.5553         0.79679         0.97652
v  FourierNb             0.0037194               1         0.39528         0.12374
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.003896     7.3035e-005      0.00019489

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.01          306.21
v  Yplus               0          2.9517         0.63527         0.49337


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69334            2.14          1.1921          1.1003


 INSTANT    0.465000000E-02   TIME STEP NUMBER             465
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925044E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18078E-01 0.46850E+01
   Friction velocity        uk    :  0.18078E-01 0.46810E+01
   Dimensionless distance   yplus :  0.12257E-01 0.29513E+01
   Friction thermal sca.    tstar :  0.90440E+00 0.14767E+03
   Rough dim-less th. sca.  tplus :  0.86833E-02 0.20907E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27794E+00       9   0.50329E-05   0.14430E+01 0.19545E+02 
c  Velocity[X]                                      0.60999E+00 
c  Velocity[Y]                                      0.39688E+00 
c  Velocity[Z]                                      0.43614E+00 
c  Pressure     0.10581E-04      17   0.17753E-03   0.10428E-01 0.17838E+02 
c  k            0.10791E-01      11   0.13122E-04   0.20340E-01 0.43753E+02 
c  omega        0.27922E+07       1   0.64364E-07   0.19778E+08 0.70064E+00 
c  TempK        0.99493E+04       6   0.35174E-05   0.27242E+02 0.18826E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4346e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.278          19.309       0.0034583       -0.011541
v  Velocity[Y]             -15.856          15.146         0.12483         0.17139
v  Velocity[Z]             -25.889          12.372          -1.665         -0.5102
v  ǁVelocityǁ         0.00049835          26.061          7.7759          6.7801
v  Pressure                -502.79          210.36          32.845          35.747
v  k                   1.0113e-010            7.25         0.14451         0.28494
v  omega                    57.502     2.7316e+008     1.2912e+006           76882
v  TempK                     298.4          363.17          332.68          337.75
v  TurbVisc            2.5346e-018      0.00075405     3.5338e-005      0.00012323
v  CourantNb            0.00013753          1.5541         0.79677         0.97652
v  FourierNb             0.0037199               1         0.39535         0.12389
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037874     7.3033e-005      0.00019489

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.01          306.21
v  Yplus               0          2.9513         0.63527         0.49337


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69574          2.1388          1.1921          1.1004


 INSTANT    0.466000000E-02   TIME STEP NUMBER             466
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925207E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18062E-01 0.46849E+01
   Friction velocity        uk    :  0.18062E-01 0.46809E+01
   Dimensionless distance   yplus :  0.12246E-01 0.29510E+01
   Friction thermal sca.    tstar :  0.91122E+00 0.14780E+03
   Rough dim-less th. sca.  tplus :  0.86752E-02 0.20905E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27798E+00       9   0.50446E-05   0.14522E+01 0.19623E+02 
c  Velocity[X]                                      0.61235E+00 
c  Velocity[Y]                                      0.40228E+00 
c  Velocity[Z]                                      0.43757E+00 
c  Pressure     0.10415E-04      17   0.17006E-03   0.10263E-01 0.19610E+02 
c  k            0.10826E-01      11   0.13194E-04   0.20418E-01 0.43736E+02 
c  omega        0.27922E+07       1   0.59729E-07   0.11013E+08 0.54986E+00 
c  TempK        0.99514E+04       6   0.35082E-05   0.27024E+02 0.18736E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4403e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.278          19.309       0.0033838       -0.011551
v  Velocity[Y]             -15.788          15.137         0.12524         0.17195
v  Velocity[Z]             -25.884          12.391         -1.6649        -0.51017
v  ǁVelocityǁ         0.00048599          26.055           7.776          6.7801
v  Pressure                 -502.6          210.25          32.731          35.632
v  k                   1.0111e-010          7.2457         0.14479          0.2857
v  omega                    57.501     2.7316e+008     1.2912e+006           76882
v  TempK                     298.4          363.17          332.71          337.79
v  TurbVisc            2.5342e-018       0.0007581     3.5411e-005      0.00012352
v  CourantNb            0.00013791          1.5527         0.79676         0.97651
v  FourierNb             0.0037205               1         0.39542         0.12404
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036784     7.3032e-005       0.0001949

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.01          306.21
v  Yplus               0           2.951         0.63527         0.49338


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62341          2.1374          1.1922          1.1006


 INSTANT    0.467000000E-02   TIME STEP NUMBER             467
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925012E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18054E-01 0.46848E+01
   Friction velocity        uk    :  0.18054E-01 0.46809E+01
   Dimensionless distance   yplus :  0.12241E-01 0.29507E+01
   Friction thermal sca.    tstar :  0.91794E+00 0.14787E+03
   Rough dim-less th. sca.  tplus :  0.86713E-02 0.20903E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27802E+00       9   0.50448E-05   0.14527E+01 0.19594E+02 
c  Velocity[X]                                      0.61437E+00 
c  Velocity[Y]                                      0.39923E+00 
c  Velocity[Z]                                      0.43910E+00 
c  Pressure     0.10210E-04      17   0.16884E-03   0.10059E-01 0.18027E+02 
c  k            0.10861E-01      11   0.13222E-04   0.20474E-01 0.43702E+02 
c  omega        0.27922E+07       1   0.55863E-07   0.41060E+07 0.38352E+00 
c  TempK        0.99535E+04       6   0.34990E-05   0.26809E+02 0.18649E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4463e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.278          19.308       0.0033079       -0.011562
v  Velocity[Y]             -15.738          15.129         0.12565         0.17252
v  Velocity[Z]             -25.878          12.409         -1.6649        -0.51014
v  ǁVelocityǁ         0.00047428           26.05          7.7761          6.7802
v  Pressure                -502.44          210.15          32.628          35.529
v  k                    1.011e-010           7.241         0.14508         0.28646
v  omega                    57.501     2.7316e+008     1.2912e+006           76883
v  TempK                     298.4          363.17          332.73          337.83
v  TurbVisc            2.5337e-018      0.00076208     3.5483e-005      0.00012381
v  CourantNb            0.00013837          1.5513         0.79674         0.97651
v  FourierNb             0.0037211               1         0.39549         0.12418
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035709     7.3029e-005      0.00019491

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.01          306.21
v  Yplus               0          2.9507         0.63526         0.49338


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81134           2.136          1.1922          1.1007


 INSTANT    0.468000000E-02   TIME STEP NUMBER             468
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925181E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18049E-01 0.46848E+01
   Friction velocity        uk    :  0.18049E-01 0.46808E+01
   Dimensionless distance   yplus :  0.12237E-01 0.29504E+01
   Friction thermal sca.    tstar :  0.92453E+00 0.14791E+03
   Rough dim-less th. sca.  tplus :  0.86689E-02 0.20901E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27806E+00       9   0.50539E-05   0.14596E+01 0.19677E+02 
c  Velocity[X]                                      0.61720E+00 
c  Velocity[Y]                                      0.40130E+00 
c  Velocity[Z]                                      0.44110E+00 
c  Pressure     0.10071E-04      17   0.16561E-03   0.99202E-02 0.18624E+02 
c  k            0.10896E-01      11   0.13266E-04   0.20524E-01 0.43660E+02 
c  omega        0.27922E+07       1   0.58277E-07   0.68735E+07 0.45729E+00 
c  TempK        0.99555E+04       6   0.34899E-05   0.26599E+02 0.18563E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.452e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.277          19.308       0.0032291       -0.011576
v  Velocity[Y]              -15.74          15.179         0.12606         0.17308
v  Velocity[Z]             -25.873          12.427         -1.6648        -0.51011
v  ǁVelocityǁ          0.0004622          26.044          7.7761          6.7803
v  Pressure                -502.29          210.04          32.522          35.423
v  k                   1.0108e-010           7.236         0.14537         0.28723
v  omega                      57.5     2.7317e+008     1.2912e+006           76883
v  TempK                     298.4          363.17          332.76          337.87
v  TurbVisc            2.5333e-018      0.00076639     3.5556e-005       0.0001241
v  CourantNb             0.0001388          1.5499         0.79672         0.97651
v  FourierNb             0.0037217               1         0.39556         0.12433
v  total_pressure      1.0082e+005     1.0154e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034658     7.3027e-005      0.00019492

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.02          306.22
v  Yplus               0          2.9504         0.63526         0.49339


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60635          2.1347          1.1923          1.1008


 INSTANT    0.469000000E-02   TIME STEP NUMBER             469
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925202E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18038E-01 0.46847E+01
   Friction velocity        uk    :  0.18038E-01 0.46807E+01
   Dimensionless distance   yplus :  0.12230E-01 0.29500E+01
   Friction thermal sca.    tstar :  0.93101E+00 0.14800E+03
   Rough dim-less th. sca.  tplus :  0.86637E-02 0.20898E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27810E+00       9   0.50691E-05   0.14731E+01 0.19818E+02 
c  Velocity[X]                                      0.62214E+00 
c  Velocity[Y]                                      0.40757E+00 
c  Velocity[Z]                                      0.44336E+00 
c  Pressure     0.10301E-04      17   0.16700E-03   0.10145E-01 0.19124E+02 
c  k            0.10931E-01      11   0.13300E-04   0.20579E-01 0.43647E+02 
c  omega        0.27922E+07       1   0.65667E-07   0.20556E+08 0.71591E+00 
c  TempK        0.99575E+04       6   0.34809E-05   0.26392E+02 0.18477E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4577e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.277          19.307         0.00315       -0.011592
v  Velocity[Y]             -15.841          15.183         0.12647         0.17365
v  Velocity[Z]             -25.867          12.443         -1.6647        -0.51007
v  ǁVelocityǁ         0.00045077          26.039          7.7762          6.7803
v  Pressure                -502.16          209.93          32.413          35.313
v  k                   1.0106e-010           7.231         0.14566         0.28799
v  omega                      57.5     2.7317e+008     1.2912e+006           76883
v  TempK                     298.4          363.17          332.79          337.92
v  TurbVisc            2.5329e-018      0.00077153     3.5628e-005      0.00012439
v  CourantNb            0.00013924          1.5485         0.79671         0.97651
v  FourierNb             0.0037222               1         0.39562         0.12448
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035672     7.3025e-005      0.00019492

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.02          306.22
v  Yplus               0            2.95         0.63526         0.49339


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83052          2.1333          1.1923           1.101


 INSTANT    0.470000000E-02   TIME STEP NUMBER             470
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925246E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18025E-01 0.46846E+01
   Friction velocity        uk    :  0.18025E-01 0.46806E+01
   Dimensionless distance   yplus :  0.12221E-01 0.29497E+01
   Friction thermal sca.    tstar :  0.93736E+00 0.14810E+03
   Rough dim-less th. sca.  tplus :  0.86578E-02 0.20896E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27814E+00       9   0.50885E-05   0.14833E+01 0.19855E+02 
c  Velocity[X]                                      0.62608E+00 
c  Velocity[Y]                                      0.40905E+00 
c  Velocity[Z]                                      0.44820E+00 
c  Pressure     0.10881E-04      17   0.17215E-03   0.10715E-01 0.20323E+02 
c  k            0.10966E-01      11   0.13372E-04   0.20702E-01 0.43734E+02 
c  omega        0.27922E+07       1   0.66093E-07   0.22057E+08 0.73558E+00 
c  TempK        0.99596E+04       6   0.34720E-05   0.26190E+02 0.18392E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4633e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.277          19.306        0.003069        -0.01161
v  Velocity[Y]             -15.896          15.105         0.12688         0.17422
v  Velocity[Z]             -25.861          12.458         -1.6647        -0.51004
v  ǁVelocityǁ         0.00043988          26.033          7.7762          6.7804
v  Pressure                -502.05          209.82          32.296          35.196
v  k                   1.0105e-010           7.226         0.14595         0.28875
v  omega                      57.5     2.7317e+008     1.2912e+006           76883
v  TempK                    298.41          363.17          332.81          337.96
v  TurbVisc            2.5325e-018      0.00077701     3.5701e-005      0.00012468
v  CourantNb            0.00013965          1.5472         0.79669          0.9765
v  FourierNb             0.0037227               1         0.39569         0.12462
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035937     7.3023e-005      0.00019493

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.02          306.22
v  Yplus               0          2.9497         0.63526         0.49339


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44178           2.132          1.1924          1.1011


 INSTANT    0.471000000E-02   TIME STEP NUMBER             471
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925057E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18016E-01 0.46846E+01
   Friction velocity        uk    :  0.18016E-01 0.46806E+01
   Dimensionless distance   yplus :  0.12215E-01 0.29493E+01
   Friction thermal sca.    tstar :  0.94360E+00 0.14818E+03
   Rough dim-less th. sca.  tplus :  0.86533E-02 0.20893E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27818E+00       9   0.51111E-05   0.14965E+01 0.19911E+02 
c  Velocity[X]                                      0.63065E+00 
c  Velocity[Y]                                      0.41257E+00 
c  Velocity[Z]                                      0.45324E+00 
c  Pressure     0.10949E-04      17   0.17276E-03   0.10780E-01 0.20139E+02 
c  k            0.11001E-01      11   0.13454E-04   0.20804E-01 0.43785E+02 
c  omega        0.27922E+07       1   0.60051E-07   0.11293E+08 0.55259E+00 
c  TempK        0.99616E+04       6   0.34631E-05   0.25988E+02 0.18308E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4697e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.276          19.305       0.0029858        -0.01163
v  Velocity[Y]             -15.819          15.097         0.12728          0.1748
v  Velocity[Z]             -25.855          12.472         -1.6646        -0.51001
v  ǁVelocityǁ          0.0004286          26.027          7.7763          6.7805
v  Pressure                -501.98           209.7          32.179          35.079
v  k                   1.0103e-010          7.2211         0.14624          0.2895
v  omega                    57.499     2.7317e+008     1.2912e+006           76884
v  TempK                    298.41          363.17          332.84             338
v  TurbVisc             2.532e-018      0.00078249     3.5773e-005      0.00012497
v  CourantNb            0.00014003          1.5457         0.79667          0.9765
v  FourierNb             0.0037232               1         0.39576         0.12477
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036229     7.3022e-005      0.00019494

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.02          306.22
v  Yplus               0          2.9493         0.63525         0.49339


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72097          2.1305          1.1924          1.1013


 INSTANT    0.472000000E-02   TIME STEP NUMBER             472
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925074E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18016E-01 0.46845E+01
   Friction velocity        uk    :  0.18016E-01 0.46805E+01
   Dimensionless distance   yplus :  0.12215E-01 0.29490E+01
   Friction thermal sca.    tstar :  0.94973E+00 0.14819E+03
   Rough dim-less th. sca.  tplus :  0.86531E-02 0.20891E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27821E+00       9   0.51154E-05   0.14897E+01 0.19873E+02 
c  Velocity[X]                                      0.63449E+00 
c  Velocity[Y]                                      0.40947E+00 
c  Velocity[Z]                                      0.44575E+00 
c  Pressure     0.10680E-04      17   0.17121E-03   0.10513E-01 0.20492E+02 
c  k            0.11036E-01      11   0.13532E-04   0.20880E-01 0.43784E+02 
c  omega        0.27922E+07       1   0.55953E-07   0.39930E+07 0.38087E+00 
c  TempK        0.99635E+04       6   0.34543E-05   0.25792E+02 0.18226E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4762e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.276          19.305       0.0029027        -0.01165
v  Velocity[Y]             -15.762          15.089         0.12769         0.17537
v  Velocity[Z]             -25.849          12.484         -1.6645        -0.50998
v  ǁVelocityǁ         0.00041763          26.022          7.7763          6.7805
v  Pressure                -501.92          209.58           32.06           34.96
v  k                   1.0101e-010          7.2164         0.14653         0.29026
v  omega                    57.499     2.7317e+008     1.2912e+006           76884
v  TempK                    298.41          363.17          332.86          338.04
v  TurbVisc            2.5316e-018      0.00078797     3.5846e-005      0.00012525
v  CourantNb            0.00014043          1.5441         0.79666         0.97649
v  FourierNb             0.0037237               1         0.39583         0.12492
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036547     7.3021e-005      0.00019495

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.03          306.22
v  Yplus               0           2.949         0.63524         0.49339


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59297           2.129          1.1925          1.1014


 INSTANT    0.473000000E-02   TIME STEP NUMBER             473
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925057E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18015E-01 0.46844E+01
   Friction velocity        uk    :  0.18015E-01 0.46804E+01
   Dimensionless distance   yplus :  0.12214E-01 0.29487E+01
   Friction thermal sca.    tstar :  0.95575E+00 0.14819E+03
   Rough dim-less th. sca.  tplus :  0.86527E-02 0.20889E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27825E+00       9   0.51298E-05   0.15022E+01 0.19936E+02 
c  Velocity[X]                                      0.64075E+00 
c  Velocity[Y]                                      0.41139E+00 
c  Velocity[Z]                                      0.45008E+00 
c  Pressure     0.10969E-04      17   0.17172E-03   0.10795E-01 0.20195E+02 
c  k            0.11071E-01      11   0.13600E-04   0.20961E-01 0.43758E+02 
c  omega        0.27922E+07       1   0.57118E-07   0.54432E+07 0.41989E+00 
c  TempK        0.99655E+04       6   0.34455E-05   0.25597E+02 0.18145E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4825e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.275          19.304       0.0028172       -0.011672
v  Velocity[Y]             -15.758          15.082          0.1281         0.17595
v  Velocity[Z]             -25.844          12.495         -1.6644        -0.50995
v  ǁVelocityǁ         0.00040689          26.016          7.7764          6.7806
v  Pressure                -501.89          209.46          31.943          34.843
v  k                   1.0099e-010          7.2122         0.14682         0.29102
v  omega                    57.499     2.7317e+008     1.2912e+006           76884
v  TempK                    298.41          363.17          332.89          338.08
v  TurbVisc            2.5312e-018      0.00079342     3.5918e-005      0.00012554
v  CourantNb            0.00014082          1.5426         0.79664         0.97649
v  FourierNb             0.0037242               1          0.3959         0.12506
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036915      7.302e-005      0.00019496

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.03          306.22
v  Yplus               0          2.9487         0.63524         0.49339


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40343          2.1275          1.1925          1.1016


 INSTANT    0.474000000E-02   TIME STEP NUMBER             474
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925085E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18011E-01 0.46844E+01
   Friction velocity        uk    :  0.18011E-01 0.46804E+01
   Dimensionless distance   yplus :  0.12212E-01 0.29484E+01
   Friction thermal sca.    tstar :  0.96166E+00 0.14822E+03
   Rough dim-less th. sca.  tplus :  0.86510E-02 0.20886E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27829E+00       9   0.51402E-05   0.15157E+01 0.20062E+02 
c  Velocity[X]                                      0.64689E+00 
c  Velocity[Y]                                      0.41445E+00 
c  Velocity[Z]                                      0.45432E+00 
c  Pressure     0.11002E-04      17   0.16989E-03   0.10827E-01 0.19975E+02 
c  k            0.11106E-01      11   0.13656E-04   0.21060E-01 0.43749E+02 
c  omega        0.27922E+07       1   0.62990E-07   0.13214E+08 0.58174E+00 
c  TempK        0.99675E+04       6   0.34368E-05   0.25407E+02 0.18065E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4886e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.275          19.303       0.0027318       -0.011698
v  Velocity[Y]             -15.855           15.16         0.12851         0.17653
v  Velocity[Z]             -25.838          12.505         -1.6643        -0.50992
v  ǁVelocityǁ         0.00039631           26.01          7.7764          6.7806
v  Pressure                -501.86          209.35           31.83          34.729
v  k                   1.0098e-010          7.2083         0.14711         0.29178
v  omega                    57.498     2.7317e+008     1.2912e+006           76885
v  TempK                    298.41          363.17          332.92          338.13
v  TurbVisc            2.5308e-018      0.00079881      3.599e-005      0.00012582
v  CourantNb             0.0001412          1.5412         0.79662         0.97649
v  FourierNb             0.0037247               1         0.39596         0.12521
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.003728     7.3018e-005      0.00019497

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.03          306.23
v  Yplus               0          2.9484         0.63523         0.49338


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71485          2.1261          1.1926          1.1017


 INSTANT    0.475000000E-02   TIME STEP NUMBER             475
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925086E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18008E-01 0.46843E+01
   Friction velocity        uk    :  0.18008E-01 0.46803E+01
   Dimensionless distance   yplus :  0.12210E-01 0.29480E+01
   Friction thermal sca.    tstar :  0.96745E+00 0.14825E+03
   Rough dim-less th. sca.  tplus :  0.86493E-02 0.20884E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27832E+00       9   0.51690E-05   0.15357E+01 0.20221E+02 
c  Velocity[X]                                      0.65554E+00 
c  Velocity[Y]                                      0.42199E+00 
c  Velocity[Z]                                      0.45820E+00 
c  Pressure     0.11479E-04      17   0.16963E-03   0.11294E-01 0.20469E+02 
c  k            0.11141E-01      11   0.13648E-04   0.21095E-01 0.43722E+02 
c  omega        0.27922E+07       1   0.67187E-07   0.22860E+08 0.74732E+00 
c  TempK        0.99694E+04       6   0.34281E-05   0.25222E+02 0.17987E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4947e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.274          19.302       0.0026466       -0.011724
v  Velocity[Y]             -15.907          15.092         0.12891         0.17711
v  Velocity[Z]             -25.832          12.513         -1.6642         -0.5099
v  ǁVelocityǁ         0.00038614          26.005          7.7765          6.7806
v  Pressure                -501.86          209.23          31.712          34.612
v  k                   1.0096e-010          7.2049          0.1474         0.29254
v  omega                    57.498     2.7317e+008     1.2912e+006           76885
v  TempK                    298.41          363.17          332.94          338.17
v  TurbVisc            2.5303e-018      0.00080221     3.6062e-005      0.00012611
v  CourantNb            0.00014157          1.5397         0.79661         0.97648
v  FourierNb             0.0037251               1         0.39603         0.12536
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037639     7.3016e-005      0.00019498

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.03          306.23
v  Yplus               0           2.948         0.63523         0.49338


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.32494          2.1247          1.1926          1.1018


 INSTANT    0.476000000E-02   TIME STEP NUMBER             476
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925108E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18007E-01 0.46843E+01
   Friction velocity        uk    :  0.18007E-01 0.46803E+01
   Dimensionless distance   yplus :  0.12209E-01 0.29476E+01
   Friction thermal sca.    tstar :  0.97315E+00 0.14826E+03
   Rough dim-less th. sca.  tplus :  0.86489E-02 0.20881E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27836E+00       9   0.51922E-05   0.15481E+01 0.20253E+02 
c  Velocity[X]                                      0.66135E+00 
c  Velocity[Y]                                      0.42449E+00 
c  Velocity[Z]                                      0.46224E+00 
c  Pressure     0.11414E-04      18   0.16972E-03   0.11228E-01 0.22347E+02 
c  k            0.11176E-01      11   0.13641E-04   0.21127E-01 0.43702E+02 
c  omega        0.27922E+07       1   0.63447E-07   0.16331E+08 0.64347E+00 
c  TempK        0.99713E+04       6   0.34195E-05   0.25040E+02 0.17910E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5015e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.273          19.301       0.0025593        -0.01175
v  Velocity[Y]             -15.827           15.06         0.12932         0.17769
v  Velocity[Z]             -25.826          12.519         -1.6641        -0.50987
v  ǁVelocityǁ         0.00037577          25.999          7.7765          6.7806
v  Pressure                 -501.9           209.1          31.581          34.482
v  k                   1.0094e-010          7.2021         0.14769          0.2933
v  omega                    57.498     2.7317e+008     1.2912e+006           76885
v  TempK                    298.42          363.17          332.97          338.21
v  TurbVisc            2.5299e-018      0.00080536     3.6134e-005      0.00012639
v  CourantNb            0.00014192          1.5381         0.79659         0.97648
v  FourierNb             0.0037257               1          0.3961          0.1255
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037991     7.3014e-005      0.00019499

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.04          306.23
v  Yplus               0          2.9476         0.63522         0.49338


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58957          2.1231          1.1927           1.102


 INSTANT    0.477000000E-02   TIME STEP NUMBER             477
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925067E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18012E-01 0.46842E+01
   Friction velocity        uk    :  0.18012E-01 0.46802E+01
   Dimensionless distance   yplus :  0.12212E-01 0.29473E+01
   Friction thermal sca.    tstar :  0.97875E+00 0.14822E+03
   Rough dim-less th. sca.  tplus :  0.86512E-02 0.20879E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27839E+00       9   0.52043E-05   0.15400E+01 0.20192E+02 
c  Velocity[X]                                      0.66376E+00 
c  Velocity[Y]                                      0.42014E+00 
c  Velocity[Z]                                      0.45612E+00 
c  Pressure     0.11314E-04      17   0.17243E-03   0.11126E-01 0.22357E+02 
c  k            0.11211E-01      11   0.13609E-04   0.21167E-01 0.43681E+02 
c  omega        0.27922E+07       1   0.56376E-07   0.42313E+07 0.37695E+00 
c  TempK        0.99733E+04       6   0.34109E-05   0.24861E+02 0.17835E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5085e-007                             8


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.273          19.299       0.0024685       -0.011777
v  Velocity[Y]             -15.765          15.053         0.12973         0.17827
v  Velocity[Z]              -25.82          12.524          -1.664        -0.50984
v  ǁVelocityǁ         0.00036602          25.993          7.7766          6.7807
v  Pressure                -501.95          208.97           31.45          34.351
v  k                   1.0093e-010          7.1999         0.14798         0.29406
v  omega                    57.497     2.7317e+008     1.2912e+006           76886
v  TempK                    298.42          363.17          332.99          338.25
v  TurbVisc            2.5295e-018      0.00080839     3.6206e-005      0.00012667
v  CourantNb            0.00014229          1.5365         0.79657         0.97647
v  FourierNb             0.0037263               1         0.39616         0.12565
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038379     7.3012e-005        0.000195

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.04          306.23
v  Yplus               0          2.9473         0.63521         0.49337


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63449          2.1215          1.1927          1.1021


 INSTANT    0.478000000E-02   TIME STEP NUMBER             478
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925019E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18017E-01 0.46841E+01
   Friction velocity        uk    :  0.18017E-01 0.46802E+01
   Dimensionless distance   yplus :  0.12216E-01 0.29470E+01
   Friction thermal sca.    tstar :  0.98425E+00 0.14818E+03
   Rough dim-less th. sca.  tplus :  0.86539E-02 0.20877E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27843E+00       9   0.52103E-05   0.15444E+01 0.20228E+02 
c  Velocity[X]                                      0.66702E+00 
c  Velocity[Y]                                      0.42145E+00 
c  Velocity[Z]                                      0.45596E+00 
c  Pressure     0.11099E-04      17   0.17681E-03   0.10913E-01 0.21831E+02 
c  k            0.11245E-01      11   0.13558E-04   0.21202E-01 0.43652E+02 
c  omega        0.27922E+07       1   0.55853E-07   0.36354E+07 0.35787E+00 
c  TempK        0.99752E+04       6   0.34024E-05   0.24683E+02 0.17761E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5151e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.272          19.298       0.0023764       -0.011805
v  Velocity[Y]             -15.756          15.047         0.13014         0.17886
v  Velocity[Z]             -25.815          12.528         -1.6639        -0.50981
v  ǁVelocityǁ         0.00035595          25.988          7.7766          6.7807
v  Pressure                -502.02          208.84          31.323          34.225
v  k                   1.0091e-010          7.1983         0.14827         0.29482
v  omega                    57.497     2.7318e+008     1.2912e+006           76886
v  TempK                    298.42          363.17          333.02          338.29
v  TurbVisc            2.5291e-018      0.00081133     3.6278e-005      0.00012696
v  CourantNb            0.00014263          1.5349         0.79655         0.97647
v  FourierNb             0.0037271               1         0.39623          0.1258
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038972     7.3011e-005      0.00019501

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.04          306.23
v  Yplus               0           2.947          0.6352         0.49337


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60141            2.12          1.1928          1.1023


 INSTANT    0.479000000E-02   TIME STEP NUMBER             479
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925063E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18021E-01 0.46841E+01
   Friction velocity        uk    :  0.18021E-01 0.46801E+01
   Dimensionless distance   yplus :  0.12219E-01 0.29467E+01
   Friction thermal sca.    tstar :  0.98966E+00 0.14814E+03
   Rough dim-less th. sca.  tplus :  0.86559E-02 0.20875E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27846E+00       9   0.52204E-05   0.15523E+01 0.20298E+02 
c  Velocity[X]                                      0.67136E+00 
c  Velocity[Y]                                      0.42248E+00 
c  Velocity[Z]                                      0.45843E+00 
c  Pressure     0.11286E-04      17   0.17800E-03   0.11094E-01 0.21045E+02 
c  k            0.11280E-01      11   0.13565E-04   0.21244E-01 0.43621E+02 
c  omega        0.27922E+07       1   0.57983E-07   0.62251E+07 0.42200E+00 
c  TempK        0.99771E+04       6   0.33939E-05   0.24506E+02 0.17688E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5215e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.271          19.297       0.0022826       -0.011835
v  Velocity[Y]              -15.85           15.04         0.13054         0.17944
v  Velocity[Z]             -25.809           12.53         -1.6639        -0.50978
v  ǁVelocityǁ         0.00034677          25.983          7.7767          6.7807
v  Pressure                 -502.1          208.72          31.201          34.104
v  k                   1.0089e-010          7.1972         0.14856         0.29558
v  omega                    57.497     2.7318e+008     1.2912e+006           76886
v  TempK                    298.42          363.17          333.04          338.33
v  TurbVisc            2.5286e-018      0.00081419      3.635e-005      0.00012724
v  CourantNb            0.00014299          1.5334         0.79654         0.97647
v  FourierNb             0.0037278               1         0.39629         0.12594
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039626     7.3009e-005      0.00019502

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.04          306.23
v  Yplus               0          2.9467          0.6352         0.49336


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.623          2.1185          1.1928          1.1024


 INSTANT    0.480000000E-02   TIME STEP NUMBER             480
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925227E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18027E-01 0.46841E+01
   Friction velocity        uk    :  0.18027E-01 0.46801E+01
   Dimensionless distance   yplus :  0.12222E-01 0.29464E+01
   Friction thermal sca.    tstar :  0.99496E+00 0.14810E+03
   Rough dim-less th. sca.  tplus :  0.86584E-02 0.20872E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27849E+00       9   0.52422E-05   0.15616E+01 0.20409E+02 
c  Velocity[X]                                      0.67335E+00 
c  Velocity[Y]                                      0.42584E+00 
c  Velocity[Z]                                      0.46244E+00 
c  Pressure     0.12777E-04      17   0.17980E-03   0.12557E-01 0.20966E+02 
c  k            0.11315E-01      11   0.13542E-04   0.21290E-01 0.43586E+02 
c  omega        0.27922E+07       1   0.66793E-07   0.22147E+08 0.72507E+00 
c  TempK        0.99789E+04       6   0.33853E-05   0.24331E+02 0.17616E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5278e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.27          19.296       0.0021906       -0.011865
v  Velocity[Y]             -15.899          15.033         0.13094         0.18003
v  Velocity[Z]             -25.804           12.53         -1.6638        -0.50976
v  ǁVelocityǁ          0.0003376          25.977          7.7767          6.7807
v  Pressure                -502.19          208.59           31.08          33.983
v  k                   1.0088e-010          7.1969         0.14886         0.29634
v  omega                    57.496     2.7318e+008     1.2912e+006           76886
v  TempK                    298.42          363.17          333.07          338.37
v  TurbVisc            2.5282e-018      0.00081698     3.6422e-005      0.00012752
v  CourantNb             0.0001433          1.5319         0.79652         0.97646
v  FourierNb             0.0037284               1         0.39636         0.12609
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0040273     7.3007e-005      0.00019503

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.05          306.23
v  Yplus               0          2.9464         0.63519         0.49336


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64275          2.1171          1.1929          1.1026


 INSTANT    0.481000000E-02   TIME STEP NUMBER             481
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925215E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18034E-01 0.46840E+01
   Friction velocity        uk    :  0.18034E-01 0.46800E+01
   Dimensionless distance   yplus :  0.12227E-01 0.29460E+01
   Friction thermal sca.    tstar :  0.10002E+01 0.14804E+03
   Rough dim-less th. sca.  tplus :  0.86618E-02 0.20870E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27852E+00       9   0.52445E-05   0.15731E+01 0.20531E+02 
c  Velocity[X]                                      0.67812E+00 
c  Velocity[Y]                                      0.43359E+00 
c  Velocity[Z]                                      0.46138E+00 
c  Pressure     0.13201E-04      17   0.17603E-03   0.12973E-01 0.21259E+02 
c  k            0.11350E-01      11   0.13498E-04   0.21335E-01 0.43556E+02 
c  omega        0.27922E+07       1   0.66994E-07   0.24496E+08 0.76518E+00 
c  TempK        0.99808E+04       6   0.33769E-05   0.24158E+02 0.17544E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5348e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.269          19.295       0.0020984       -0.011897
v  Velocity[Y]             -15.814          15.026         0.13135         0.18062
v  Velocity[Z]             -25.798          12.528         -1.6637        -0.50973
v  ǁVelocityǁ         0.00032846          25.972          7.7768          6.7807
v  Pressure                -502.32          208.47          30.957          33.861
v  k                   1.0086e-010          7.1971         0.14915          0.2971
v  omega                    57.496     2.7318e+008     1.2912e+006           76887
v  TempK                    298.42          363.17          333.09          338.41
v  TurbVisc            2.5278e-018      0.00082063     3.6494e-005       0.0001278
v  CourantNb            0.00014362          1.5303         0.79651         0.97646
v  FourierNb             0.0037286               1         0.39643         0.12623
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0040748     7.3005e-005      0.00019504

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.05          306.24
v  Yplus               0           2.946         0.63519         0.49335


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55568          2.1155          1.1929          1.1027


 INSTANT    0.482000000E-02   TIME STEP NUMBER             482
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925204E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18045E-01 0.46840E+01
   Friction velocity        uk    :  0.18045E-01 0.46800E+01
   Dimensionless distance   yplus :  0.12235E-01 0.29457E+01
   Friction thermal sca.    tstar :  0.10053E+01 0.14795E+03
   Rough dim-less th. sca.  tplus :  0.86674E-02 0.20867E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27856E+00       9   0.52520E-05   0.15734E+01 0.20460E+02 
c  Velocity[X]                                      0.68144E+00 
c  Velocity[Y]                                      0.42710E+00 
c  Velocity[Z]                                      0.46487E+00 
c  Pressure     0.12739E-04      18   0.17615E-03   0.12517E-01 0.23331E+02 
c  k            0.11385E-01      11   0.13500E-04   0.21373E-01 0.43512E+02 
c  omega        0.27922E+07       1   0.57959E-07   0.70469E+07 0.44051E+00 
c  TempK        0.99826E+04       6   0.33684E-05   0.23989E+02 0.17474E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5419e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.268          19.294       0.0020024       -0.011929
v  Velocity[Y]             -15.747           15.02         0.13175         0.18121
v  Velocity[Z]             -25.792          12.525         -1.6636        -0.50971
v  ǁVelocityǁ         0.00031914          25.966          7.7768          6.7807
v  Pressure                -502.47          208.33           30.82          33.726
v  k                   1.0084e-010           7.198         0.14944         0.29786
v  omega                    57.496     2.7318e+008     1.2912e+006           76887
v  TempK                    298.42          363.17          333.12          338.45
v  TurbVisc            2.5274e-018      0.00082432     3.6567e-005      0.00012809
v  CourantNb            0.00014394          1.5286         0.79649         0.97646
v  FourierNb             0.0037287               1         0.39649         0.12638
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0040416     7.3003e-005      0.00019505

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.05          306.24
v  Yplus               0          2.9457         0.63518         0.49335


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46454          2.1139           1.193          1.1028


 INSTANT    0.483000000E-02   TIME STEP NUMBER             483
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925043E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18057E-01 0.46839E+01
   Friction velocity        uk    :  0.18056E-01 0.46799E+01
   Dimensionless distance   yplus :  0.12243E-01 0.29454E+01
   Friction thermal sca.    tstar :  0.10103E+01 0.14786E+03
   Rough dim-less th. sca.  tplus :  0.86727E-02 0.20865E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27859E+00       9   0.52678E-05   0.15785E+01 0.20480E+02 
c  Velocity[X]                                      0.68316E+00 
c  Velocity[Y]                                      0.42655E+00 
c  Velocity[Z]                                      0.46880E+00 
c  Pressure     0.12693E-04      17   0.17995E-03   0.12470E-01 0.22362E+02 
c  k            0.11420E-01      11   0.13454E-04   0.21415E-01 0.43463E+02 
c  omega        0.27922E+07       1   0.56055E-07   0.39352E+07 0.35611E+00 
c  TempK        0.99845E+04       6   0.33599E-05   0.23825E+02 0.17405E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5487e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.267          19.293        0.001908       -0.011959
v  Velocity[Y]             -15.732          15.014         0.13215          0.1818
v  Velocity[Z]             -25.787           12.52         -1.6635        -0.50968
v  ǁVelocityǁ         0.00031143          25.961          7.7768          6.7806
v  Pressure                -502.64           208.2          30.689          33.596
v  k                   1.0083e-010          7.1994         0.14974         0.29862
v  omega                    57.495     2.7318e+008     1.2912e+006           76887
v  TempK                    298.42          363.17          333.14          338.49
v  TurbVisc             2.527e-018      0.00082798     3.6639e-005      0.00012837
v  CourantNb            0.00014428           1.527         0.79648         0.97646
v  FourierNb              0.003729               1         0.39655         0.12653
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038521        7.3e-005      0.00019506

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.05          306.24
v  Yplus               0          2.9454         0.63517         0.49334


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46779          2.1124           1.193           1.103


 INSTANT    0.484000000E-02   TIME STEP NUMBER             484
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925034E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18068E-01 0.46839E+01
   Friction velocity        uk    :  0.18068E-01 0.46799E+01
   Dimensionless distance   yplus :  0.12251E-01 0.29451E+01
   Friction thermal sca.    tstar :  0.10153E+01 0.14776E+03
   Rough dim-less th. sca.  tplus :  0.86784E-02 0.20863E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27862E+00       9   0.52717E-05   0.15768E+01 0.20536E+02 
c  Velocity[X]                                      0.68460E+00 
c  Velocity[Y]                                      0.42737E+00 
c  Velocity[Z]                                      0.46485E+00 
c  Pressure     0.11930E-04      18   0.18003E-03   0.11719E-01 0.21511E+02 
c  k            0.11454E-01      11   0.13420E-04   0.21463E-01 0.43418E+02 
c  omega        0.27922E+07       1   0.57995E-07   0.60994E+07 0.41737E+00 
c  TempK        0.99863E+04       6   0.33514E-05   0.23663E+02 0.17337E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5551e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.266          19.292       0.0018133       -0.011986
v  Velocity[Y]             -15.821          15.008         0.13255         0.18239
v  Velocity[Z]             -25.782          12.514         -1.6634        -0.50966
v  ǁVelocityǁ         0.00030296          25.956          7.7768          6.7806
v  Pressure                -502.82          208.07          30.565          33.473
v  k                   1.0081e-010          7.2014         0.15003         0.29937
v  omega                    57.495     2.7318e+008     1.2912e+006           76888
v  TempK                    298.42          363.17          333.16          338.53
v  TurbVisc            2.5265e-018       0.0008316     3.6711e-005      0.00012865
v  CourantNb            0.00014453          1.5255         0.79646         0.97646
v  FourierNb             0.0037294               1         0.39662         0.12667
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036379     7.2997e-005      0.00019507

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.06          306.24
v  Yplus               0          2.9451         0.63517         0.49334


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48892          2.1109          1.1931          1.1031


 INSTANT    0.485000000E-02   TIME STEP NUMBER             485
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925108E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18080E-01 0.46838E+01
   Friction velocity        uk    :  0.18080E-01 0.46798E+01
   Dimensionless distance   yplus :  0.12259E-01 0.29448E+01
   Friction thermal sca.    tstar :  0.10202E+01 0.14767E+03
   Rough dim-less th. sca.  tplus :  0.86842E-02 0.20861E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27864E+00       9   0.52849E-05   0.15883E+01 0.20621E+02 
c  Velocity[X]                                      0.68952E+00 
c  Velocity[Y]                                      0.43061E+00 
c  Velocity[Z]                                      0.46819E+00 
c  Pressure     0.12055E-04      18   0.18842E-03   0.11842E-01 0.21394E+02 
c  k            0.11489E-01      11   0.13398E-04   0.21498E-01 0.43367E+02 
c  omega        0.27922E+07       1   0.65218E-07   0.19983E+08 0.69358E+00 
c  TempK        0.99880E+04       6   0.33430E-05   0.23504E+02 0.17271E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5614e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.265          19.291       0.0017182       -0.012011
v  Velocity[Y]             -15.864          15.001         0.13294         0.18298
v  Velocity[Z]             -25.777          12.506         -1.6634        -0.50964
v  ǁVelocityǁ         0.00029575          25.951          7.7769          6.7805
v  Pressure                -503.01          207.94          30.441          33.351
v  k                   1.0079e-010           7.204         0.15032         0.30013
v  omega                    57.495     2.7318e+008     1.2912e+006           76888
v  TempK                    298.42          363.17          333.19          338.57
v  TurbVisc            2.5261e-018      0.00083519     3.6783e-005      0.00012893
v  CourantNb            0.00014483          1.5241         0.79645         0.97645
v  FourierNb               0.00373               1         0.39668         0.12682
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034627     7.2995e-005      0.00019508

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.06          306.24
v  Yplus               0          2.9448         0.63516         0.49333


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50855          2.1095          1.1931          1.1033


 INSTANT    0.486000000E-02   TIME STEP NUMBER             486
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925048E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18095E-01 0.46838E+01
   Friction velocity        uk    :  0.18095E-01 0.46798E+01
   Dimensionless distance   yplus :  0.12269E-01 0.29445E+01
   Friction thermal sca.    tstar :  0.10250E+01 0.14755E+03
   Rough dim-less th. sca.  tplus :  0.86914E-02 0.20859E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27867E+00       9   0.52991E-05   0.16007E+01 0.20736E+02 
c  Velocity[X]                                      0.69429E+00 
c  Velocity[Y]                                      0.43543E+00 
c  Velocity[Z]                                      0.47096E+00 
c  Pressure     0.12019E-04      18   0.18408E-03   0.11805E-01 0.20940E+02 
c  k            0.11524E-01      11   0.13339E-04   0.21523E-01 0.43318E+02 
c  omega        0.27922E+07       1   0.62606E-07   0.14282E+08 0.59332E+00 
c  TempK        0.99898E+04       6   0.33346E-05   0.23350E+02 0.17205E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5684e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.264           19.29       0.0016207       -0.012036
v  Velocity[Y]             -15.772          14.995         0.13333         0.18357
v  Velocity[Z]             -25.772          12.496         -1.6633        -0.50962
v  ǁVelocityǁ         0.00028647          25.945          7.7769          6.7805
v  Pressure                -503.22          207.82          30.321          33.231
v  k                   1.0078e-010          7.2071         0.15062         0.30089
v  omega                    57.495     2.7319e+008     1.2912e+006           76888
v  TempK                    298.42          363.17          333.21          338.62
v  TurbVisc            2.5257e-018       0.0008391     3.6855e-005      0.00012921
v  CourantNb            0.00014507          1.5224         0.79643         0.97645
v  FourierNb             0.0037304               1         0.39675         0.12697
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034456     7.2992e-005      0.00019509

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.06          306.24
v  Yplus               0          2.9445         0.63516         0.49333


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66167          2.1079          1.1932          1.1034


 INSTANT    0.487000000E-02   TIME STEP NUMBER             487
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925105E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18114E-01 0.46837E+01
   Friction velocity        uk    :  0.18114E-01 0.46797E+01
   Dimensionless distance   yplus :  0.12281E-01 0.29441E+01
   Friction thermal sca.    tstar :  0.10297E+01 0.14740E+03
   Rough dim-less th. sca.  tplus :  0.87002E-02 0.20857E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27870E+00       9   0.53178E-05   0.16130E+01 0.20781E+02 
c  Velocity[X]                                      0.69993E+00 
c  Velocity[Y]                                      0.43575E+00 
c  Velocity[Z]                                      0.47735E+00 
c  Pressure     0.12616E-04      17   0.18358E-03   0.12393E-01 0.21758E+02 
c  k            0.11559E-01      11   0.13317E-04   0.21543E-01 0.43250E+02 
c  omega        0.27922E+07       1   0.61340E-07   0.12361E+08 0.55658E+00 
c  TempK        0.99916E+04       6   0.33262E-05   0.23199E+02 0.17140E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5755e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.263          19.289       0.0015218        -0.01206
v  Velocity[Y]             -15.699          14.989         0.13372         0.18417
v  Velocity[Z]             -25.766          12.485         -1.6632         -0.5096
v  ǁVelocityǁ         0.00027927           25.94          7.7769          6.7804
v  Pressure                -503.47          207.69          30.194          33.107
v  k                   1.0076e-010          7.2107         0.15091         0.30165
v  omega                    57.494     2.7319e+008     1.2912e+006           76888
v  TempK                    298.42          363.17          333.24          338.65
v  TurbVisc            2.5253e-018      0.00084474     3.6927e-005      0.00012949
v  CourantNb            0.00014543          1.5208         0.79642         0.97645
v  FourierNb             0.0037309               1         0.39681         0.12712
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034702     7.2989e-005       0.0001951

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.06          306.25
v  Yplus               0          2.9441         0.63516         0.49333


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.31216          2.1064          1.1932          1.1036


 INSTANT    0.488000000E-02   TIME STEP NUMBER             488
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925062E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18130E-01 0.46837E+01
   Friction velocity        uk    :  0.18130E-01 0.46797E+01
   Dimensionless distance   yplus :  0.12293E-01 0.29438E+01
   Friction thermal sca.    tstar :  0.10344E+01 0.14726E+03
   Rough dim-less th. sca.  tplus :  0.87082E-02 0.20854E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27873E+00       9   0.53333E-05   0.16228E+01 0.20800E+02 
c  Velocity[X]                                      0.70422E+00 
c  Velocity[Y]                                      0.43423E+00 
c  Velocity[Z]                                      0.48434E+00 
c  Pressure     0.11743E-04      18   0.18279E-03   0.11536E-01 0.22468E+02 
c  k            0.11593E-01      11   0.13258E-04   0.21575E-01 0.43192E+02 
c  omega        0.27922E+07       1   0.58954E-07   0.72129E+07 0.44883E+00 
c  TempK        0.99933E+04       6   0.33179E-05   0.23046E+02 0.17076E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5822e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.262          19.288       0.0014217       -0.012084
v  Velocity[Y]             -15.678          14.984         0.13411         0.18476
v  Velocity[Z]             -25.761          12.472         -1.6631        -0.50958
v  ǁVelocityǁ         0.00027129          25.935          7.7769          6.7803
v  Pressure                -503.73          207.56          30.063          32.978
v  k                   1.0074e-010          7.2147         0.15121          0.3024
v  omega                    57.494     2.7319e+008     1.2912e+006           76889
v  TempK                    298.42          363.17          333.26          338.69
v  TurbVisc            2.5249e-018      0.00085011        3.7e-005      0.00012977
v  CourantNb            0.00014568          1.5192          0.7964         0.97645
v  FourierNb             0.0037313               1         0.39688         0.12726
v  total_pressure      1.0082e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034866     7.2987e-005      0.00019511

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.06          306.25
v  Yplus               0          2.9438         0.63515         0.49332


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68643          2.1049          1.1933          1.1037


 INSTANT    0.489000000E-02   TIME STEP NUMBER             489
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925026E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18149E-01 0.46836E+01
   Friction velocity        uk    :  0.18149E-01 0.46796E+01
   Dimensionless distance   yplus :  0.12305E-01 0.29435E+01
   Friction thermal sca.    tstar :  0.10389E+01 0.14711E+03
   Rough dim-less th. sca.  tplus :  0.87171E-02 0.20852E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27875E+00       9   0.53510E-05   0.16151E+01 0.20819E+02 
c  Velocity[X]                                      0.70697E+00 
c  Velocity[Y]                                      0.43327E+00 
c  Velocity[Z]                                      0.47481E+00 
c  Pressure     0.11217E-04      18   0.18125E-03   0.11020E-01 0.21930E+02 
c  k            0.11628E-01      11   0.13244E-04   0.21603E-01 0.43128E+02 
c  omega        0.27922E+07       1   0.58746E-07   0.63606E+07 0.42235E+00 
c  TempK        0.99950E+04       6   0.33095E-05   0.22891E+02 0.17013E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5884e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.261          19.287       0.0013183       -0.012108
v  Velocity[Y]             -15.762          14.978         0.13449         0.18536
v  Velocity[Z]             -25.756          12.457         -1.6631        -0.50956
v  ǁVelocityǁ         0.00026494           25.93          7.7769          6.7802
v  Pressure                   -504          207.43          29.936          32.852
v  k                   1.0073e-010          7.2192          0.1515         0.30316
v  omega                    57.494     2.7319e+008     1.2912e+006           76889
v  TempK                    298.43          363.17          333.28          338.73
v  TurbVisc            2.5245e-018      0.00085521     3.7072e-005      0.00013005
v  CourantNb            0.00014598          1.5178         0.79639         0.97644
v  FourierNb             0.0037317               1         0.39694         0.12741
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034986     7.2985e-005      0.00019512

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.07          306.25
v  Yplus               0          2.9435         0.63515         0.49331


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73693          2.1035          1.1933          1.1039


 INSTANT    0.490000000E-02   TIME STEP NUMBER             490
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925068E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18168E-01 0.46836E+01
   Friction velocity        uk    :  0.18168E-01 0.46796E+01
   Dimensionless distance   yplus :  0.12318E-01 0.29432E+01
   Friction thermal sca.    tstar :  0.10435E+01 0.14696E+03
   Rough dim-less th. sca.  tplus :  0.87263E-02 0.20850E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27878E+00       9   0.53787E-05   0.16240E+01 0.20899E+02 
c  Velocity[X]                                      0.70969E+00 
c  Velocity[Y]                                      0.43555E+00 
c  Velocity[Z]                                      0.47877E+00 
c  Pressure     0.11120E-04      18   0.17968E-03   0.10924E-01 0.21359E+02 
c  k            0.11662E-01      11   0.13201E-04   0.21645E-01 0.43072E+02 
c  omega        0.27922E+07       1   0.66524E-07   0.21118E+08 0.71148E+00 
c  TempK        0.99967E+04       6   0.33012E-05   0.22741E+02 0.16951E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5945e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.259          19.286       0.0012154       -0.012131
v  Velocity[Y]             -15.799          14.972         0.13487         0.18595
v  Velocity[Z]             -25.751          12.441          -1.663        -0.50955
v  ǁVelocityǁ         0.00025819          25.925          7.7769          6.7802
v  Pressure                -504.27          207.31          29.813          32.731
v  k                   1.0071e-010           7.224          0.1518         0.30392
v  omega                    57.494     2.7319e+008     1.2912e+006           76889
v  TempK                    298.43          363.17          333.31          338.77
v  TurbVisc             2.524e-018      0.00086005     3.7144e-005      0.00013033
v  CourantNb             0.0001462          1.5164         0.79637         0.97644
v  FourierNb             0.0037321               1         0.39701         0.12756
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035039     7.2984e-005      0.00019514

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.07          306.25
v  Yplus               0          2.9432         0.63515         0.49331


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.33279          2.1022          1.1934           1.104


 INSTANT    0.491000000E-02   TIME STEP NUMBER             491
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925079E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18190E-01 0.46835E+01
   Friction velocity        uk    :  0.18190E-01 0.46795E+01
   Dimensionless distance   yplus :  0.12333E-01 0.29429E+01
   Friction thermal sca.    tstar :  0.10479E+01 0.14678E+03
   Rough dim-less th. sca.  tplus :  0.87367E-02 0.20848E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27880E+00       9   0.54758E-05   0.16285E+01 0.20962E+02 
c  Velocity[X]                                      0.71112E+00 
c  Velocity[Y]                                      0.43891E+00 
c  Velocity[Z]                                      0.47846E+00 
c  Pressure     0.11118E-04      17   0.18189E-03   0.10923E-01 0.21515E+02 
c  k            0.11697E-01      11   0.13242E-04   0.21700E-01 0.43035E+02 
c  omega        0.27922E+07       1   0.61537E-07   0.12248E+08 0.55772E+00 
c  TempK        0.99984E+04       6   0.32928E-05   0.22593E+02 0.16889E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6014e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258          19.284       0.0011096       -0.012153
v  Velocity[Y]             -15.701          14.967         0.13525         0.18654
v  Velocity[Z]             -25.746          12.423         -1.6629        -0.50953
v  ǁVelocityǁ         0.00025147          25.921          7.7769            6.78
v  Pressure                -504.58          207.18          29.687          32.607
v  k                   1.0069e-010          7.2293          0.1521         0.30467
v  omega                    57.493     2.7319e+008     1.2912e+006           76889
v  TempK                    298.43          363.17          333.33          338.81
v  TurbVisc            2.5236e-018      0.00086463     3.7217e-005      0.00013061
v  CourantNb            0.00014644          1.5148         0.79636         0.97644
v  FourierNb             0.0037327               1         0.39707         0.12771
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036148     7.2983e-005      0.00019515

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.07          306.25
v  Yplus               0          2.9429         0.63514          0.4933


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72231          2.1006          1.1934          1.1041


 INSTANT    0.492000000E-02   TIME STEP NUMBER             492
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924991E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18211E-01 0.46835E+01
   Friction velocity        uk    :  0.18211E-01 0.46795E+01
   Dimensionless distance   yplus :  0.12347E-01 0.29427E+01
   Friction thermal sca.    tstar :  0.10523E+01 0.14662E+03
   Rough dim-less th. sca.  tplus :  0.87468E-02 0.20846E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27883E+00       9   0.54910E-05   0.16297E+01 0.20939E+02 
c  Velocity[X]                                      0.71309E+00 
c  Velocity[Y]                                      0.43412E+00 
c  Velocity[Z]                                      0.48251E+00 
c  Pressure     0.11296E-04      17   0.18425E-03   0.11097E-01 0.20500E+02 
c  k            0.11731E-01      11   0.13164E-04   0.21756E-01 0.42991E+02 
c  omega        0.27922E+07       1   0.58286E-07   0.57786E+07 0.40637E+00 
c  TempK        0.10000E+05       6   0.32845E-05   0.22447E+02 0.16828E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6082e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.283       0.0010015       -0.012176
v  Velocity[Y]             -15.621          14.961         0.13562         0.18714
v  Velocity[Z]             -25.742          12.404         -1.6628        -0.50951
v  ǁVelocityǁ         0.00024492          25.916          7.7768          6.7799
v  Pressure                 -504.9          207.06          29.569          32.492
v  k                   1.0068e-010          7.2349         0.15239         0.30542
v  omega                    57.493     2.7319e+008     1.2912e+006           76890
v  TempK                    298.43          363.17          333.35          338.85
v  TurbVisc            2.5232e-018      0.00086897     3.7289e-005      0.00013089
v  CourantNb            0.00014669          1.5133         0.79634         0.97644
v  FourierNb             0.0037336               1         0.39713         0.12786
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.003729     7.2982e-005      0.00019517

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.07          306.25
v  Yplus               0          2.9427         0.63514          0.4933


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.36081          2.0991          1.1935          1.1043


 INSTANT    0.493000000E-02   TIME STEP NUMBER             493
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925163E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18236E-01 0.46834E+01
   Friction velocity        uk    :  0.18236E-01 0.46794E+01
   Dimensionless distance   yplus :  0.12364E-01 0.29424E+01
   Friction thermal sca.    tstar :  0.10567E+01 0.14642E+03
   Rough dim-less th. sca.  tplus :  0.87588E-02 0.20844E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27885E+00       9   0.54889E-05   0.16358E+01 0.21020E+02 
c  Velocity[X]                                      0.71460E+00 
c  Velocity[Y]                                      0.43736E+00 
c  Velocity[Z]                                      0.48389E+00 
c  Pressure     0.10945E-04      17   0.18412E-03   0.10753E-01 0.20806E+02 
c  k            0.11765E-01      11   0.13167E-04   0.21909E-01 0.43036E+02 
c  omega        0.27922E+07       1   0.61126E-07   0.95743E+07 0.50411E+00 
c  TempK        0.10002E+05       6   0.32762E-05   0.22300E+02 0.16767E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6146e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.282      0.00089483       -0.012199
v  Velocity[Y]             -15.591          14.956         0.13599         0.18774
v  Velocity[Z]             -25.737          12.384         -1.6628        -0.50949
v  ǁVelocityǁ         0.00023909          25.912          7.7768          6.7798
v  Pressure                -505.25          206.94          29.449          32.374
v  k                   1.0066e-010          7.2409         0.15269         0.30618
v  omega                    57.493     2.7319e+008     1.2912e+006           76890
v  TempK                    298.43          363.17          333.38          338.89
v  TurbVisc            2.5228e-018      0.00087307     3.7361e-005      0.00013117
v  CourantNb            0.00014694          1.5118         0.79633         0.97644
v  FourierNb             0.0037348               1          0.3972         0.12801
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.003789      7.298e-005      0.00019518

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.08          306.25
v  Yplus               0          2.9424         0.63513         0.49329


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90535          2.0977          1.1935          1.1044


 INSTANT    0.494000000E-02   TIME STEP NUMBER             494
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925149E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18258E-01 0.46834E+01
   Friction velocity        uk    :  0.18258E-01 0.46794E+01
   Dimensionless distance   yplus :  0.12379E-01 0.29421E+01
   Friction thermal sca.    tstar :  0.10610E+01 0.14624E+03
   Rough dim-less th. sca.  tplus :  0.87694E-02 0.20842E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27887E+00       9   0.55006E-05   0.16361E+01 0.21081E+02 
c  Velocity[X]                                      0.71602E+00 
c  Velocity[Y]                                      0.43791E+00 
c  Velocity[Z]                                      0.48218E+00 
c  Pressure     0.10536E-04      18   0.18309E-03   0.10351E-01 0.20851E+02 
c  k            0.11799E-01      11   0.13061E-04   0.21771E-01 0.42846E+02 
c  omega        0.27922E+07       1   0.61509E-07   0.10058E+08 0.51162E+00 
c  TempK        0.10003E+05       6   0.32678E-05   0.22155E+02 0.16706E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6205e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255          19.281      0.00078786        -0.01222
v  Velocity[Y]             -15.667          14.951         0.13636         0.18834
v  Velocity[Z]             -25.732          12.362         -1.6627        -0.50948
v  ǁVelocityǁ         0.00023283          25.907          7.7768          6.7797
v  Pressure                -505.61          206.81           29.33          32.256
v  k                   1.0064e-010          7.2472         0.15299         0.30693
v  omega                    57.493      2.732e+008     1.2912e+006           76890
v  TempK                    298.43          363.17           333.4          338.93
v  TurbVisc            2.5224e-018      0.00087691     3.7434e-005      0.00013144
v  CourantNb            0.00014715          1.5105         0.79631         0.97643
v  FourierNb             0.0037358               1         0.39726         0.12816
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.003742     7.2979e-005       0.0001952

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.08          306.26
v  Yplus               0          2.9421         0.63513         0.49329


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52169          2.0965          1.1936          1.1046


 INSTANT    0.495000000E-02   TIME STEP NUMBER             495
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925093E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18001E-01 0.46833E+01
   Friction velocity        uk    :  0.18001E-01 0.46793E+01
   Dimensionless distance   yplus :  0.12205E-01 0.29418E+01
   Friction thermal sca.    tstar :  0.10652E+01 0.14604E+03
   Rough dim-less th. sca.  tplus :  0.86459E-02 0.20840E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27890E+00       9   0.54993E-05   0.16371E+01 0.21110E+02 
c  Velocity[X]                                      0.71464E+00 
c  Velocity[Y]                                      0.43886E+00 
c  Velocity[Z]                                      0.48363E+00 
c  Pressure     0.10335E-04      18   0.18453E-03   0.10153E-01 0.20868E+02 
c  k            0.11833E-01      11   0.12967E-04   0.21720E-01 0.42747E+02 
c  omega        0.27922E+07       1   0.69189E-07   0.25829E+08 0.78190E+00 
c  TempK        0.10005E+05       6   0.32595E-05   0.22012E+02 0.16646E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6262e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.254          19.279      0.00068401       -0.012241
v  Velocity[Y]             -15.699          14.946         0.13673         0.18893
v  Velocity[Z]             -25.727          12.338         -1.6626        -0.50946
v  ǁVelocityǁ         0.00022789          25.902          7.7768          6.7795
v  Pressure                -505.96          206.69          29.209          32.137
v  k                   1.0063e-010          7.2538         0.15328         0.30768
v  omega                    57.492      2.732e+008     1.2912e+006           76890
v  TempK                    298.43          363.17          333.42          338.97
v  TurbVisc             2.522e-018      0.00088049     3.7506e-005      0.00013172
v  CourantNb             0.0001474          1.5092          0.7963         0.97643
v  FourierNb             0.0037361               1         0.39733         0.12831
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036963     7.2979e-005      0.00019522

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.08          306.26
v  Yplus               0          2.9418         0.63513         0.49328


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75531          2.0952          1.1936          1.1047


 INSTANT    0.496000000E-02   TIME STEP NUMBER             496
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925058E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17779E-01 0.46832E+01
   Friction velocity        uk    :  0.17778E-01 0.46793E+01
   Dimensionless distance   yplus :  0.12054E-01 0.29415E+01
   Friction thermal sca.    tstar :  0.10694E+01 0.14582E+03
   Rough dim-less th. sca.  tplus :  0.85392E-02 0.20838E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27892E+00       9   0.55047E-05   0.16404E+01 0.21131E+02 
c  Velocity[X]                                      0.71418E+00 
c  Velocity[Y]                                      0.44101E+00 
c  Velocity[Z]                                      0.48525E+00 
c  Pressure     0.10469E-04      17   0.19152E-03   0.10284E-01 0.20771E+02 
c  k            0.11867E-01      11   0.12933E-04   0.21927E-01 0.42853E+02 
c  omega        0.27922E+07       1   0.62023E-07   0.12724E+08 0.56717E+00 
c  TempK        0.10007E+05       6   0.32512E-05   0.21871E+02 0.16587E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6327e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.278      0.00057843       -0.012261
v  Velocity[Y]             -15.598          14.941         0.13709         0.18953
v  Velocity[Z]             -25.723          12.312         -1.6626        -0.50944
v  ǁVelocityǁ         0.00022235          25.897          7.7767          6.7794
v  Pressure                -506.33          206.57          29.089           32.02
v  k                   1.0061e-010          7.2607         0.15358         0.30843
v  omega                    57.492      2.732e+008     1.2912e+006           76891
v  TempK                    298.43          363.17          333.45          339.01
v  TurbVisc            2.5216e-018      0.00088379     3.7578e-005        0.000132
v  CourantNb            0.00014757          1.5077         0.79628         0.97643
v  FourierNb             0.0037358               1         0.39739         0.12846
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036524      7.298e-005      0.00019523

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.08          306.26
v  Yplus               0          2.9415         0.63512         0.49328


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48614          2.0938          1.1937          1.1049


 INSTANT    0.497000000E-02   TIME STEP NUMBER             497
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924973E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17526E-01 0.46832E+01
   Friction velocity        uk    :  0.17525E-01 0.46792E+01
   Dimensionless distance   yplus :  0.11883E-01 0.29412E+01
   Friction thermal sca.    tstar :  0.10736E+01 0.14561E+03
   Rough dim-less th. sca.  tplus :  0.84177E-02 0.20836E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27894E+00       9   0.55078E-05   0.16373E+01 0.21077E+02 
c  Velocity[X]                                      0.71496E+00 
c  Velocity[Y]                                      0.43618E+00 
c  Velocity[Z]                                      0.48612E+00 
c  Pressure     0.10376E-04      17   0.19322E-03   0.10192E-01 0.20407E+02 
c  k            0.11901E-01      11   0.12908E-04   0.22101E-01 0.43053E+02 
c  omega        0.27922E+07       1   0.57023E-07   0.37691E+07 0.35115E+00 
c  TempK        0.10008E+05       6   0.32429E-05   0.21732E+02 0.16528E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6391e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.277      0.00047356        -0.01228
v  Velocity[Y]             -15.514          14.937         0.13745         0.19013
v  Velocity[Z]             -25.718          12.285         -1.6625        -0.50943
v  ǁVelocityǁ         0.00021688          25.893          7.7767          6.7792
v  Pressure                -506.72          206.45          28.971          31.904
v  k                   1.0059e-010          7.7646         0.15388         0.30918
v  omega                    57.492      2.732e+008     1.2912e+006           76891
v  TempK                    298.43          363.17          333.47          339.05
v  TurbVisc            2.5212e-018      0.00088681     3.7651e-005      0.00013228
v  CourantNb            0.00014779          1.5062         0.79626         0.97642
v  FourierNb             0.0037355               1         0.39746         0.12862
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036114     7.2981e-005      0.00019525

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.08          306.26
v  Yplus               0          2.9412         0.63512         0.49327


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68189          2.0924          1.1937           1.105


 INSTANT    0.498000000E-02   TIME STEP NUMBER             498
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925000E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17270E-01 0.46831E+01
   Friction velocity        uk    :  0.17270E-01 0.46791E+01
   Dimensionless distance   yplus :  0.11709E-01 0.29410E+01
   Friction thermal sca.    tstar :  0.10778E+01 0.14733E+03
   Rough dim-less th. sca.  tplus :  0.82948E-02 0.20834E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27896E+00       9   0.54824E-05   0.16383E+01 0.21096E+02 
c  Velocity[X]                                      0.71603E+00 
c  Velocity[Y]                                      0.43714E+00 
c  Velocity[Z]                                      0.48516E+00 
c  Pressure     0.10286E-04      17   0.19569E-03   0.10103E-01 0.20124E+02 
c  k            0.11934E-01      10   0.13617E-04   0.21889E-01 0.42745E+02 
c  omega        0.27922E+07       1   0.56701E-07   0.35039E+07 0.34962E+00 
c  TempK        0.10010E+05       6   0.32346E-05   0.21595E+02 0.16470E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6451e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.275       0.0003663         -0.0123
v  Velocity[Y]             -15.476          14.933         0.13781         0.19074
v  Velocity[Z]             -25.714          12.256         -1.6624        -0.50941
v  ǁVelocityǁ         0.00021287          25.889          7.7766          6.7791
v  Pressure                 -507.1          206.33          28.855          31.791
v  k                   1.0058e-010          8.1731         0.15417         0.30993
v  omega                    57.492      2.732e+008     1.2912e+006           76891
v  TempK                    298.43          363.17          333.49          339.09
v  TurbVisc            2.5207e-018      0.00088954     3.7723e-005      0.00013256
v  CourantNb            0.00014802          1.5049         0.79625         0.97642
v  FourierNb             0.0037356               1         0.39752         0.12877
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035721     7.2982e-005      0.00019527

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.09          306.26
v  Yplus               0           2.941         0.63512         0.49327


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5463          2.0912          1.1938          1.1052


 INSTANT    0.499000000E-02   TIME STEP NUMBER             499
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924985E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17079E-01 0.46831E+01
   Friction velocity        uk    :  0.17079E-01 0.46791E+01
   Dimensionless distance   yplus :  0.11580E-01 0.29407E+01
   Friction thermal sca.    tstar :  0.10819E+01 0.14897E+03
   Rough dim-less th. sca.  tplus :  0.82032E-02 0.20832E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27898E+00       9   0.54805E-05   0.16435E+01 0.21142E+02 
c  Velocity[X]                                      0.71765E+00 
c  Velocity[Y]                                      0.43845E+00 
c  Velocity[Z]                                      0.48744E+00 
c  Pressure     0.10534E-04      17   0.19634E-03   0.10347E-01 0.19569E+02 
c  k            0.11968E-01      10   0.13615E-04   0.21759E-01 0.42513E+02 
c  omega        0.27922E+07       1   0.59050E-07   0.73039E+07 0.44773E+00 
c  TempK        0.10011E+05       6   0.32263E-05   0.21458E+02 0.16412E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6503e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.274      0.00025606        -0.01232
v  Velocity[Y]             -15.508          14.928         0.13817         0.19134
v  Velocity[Z]              -25.71          12.225         -1.6624        -0.50939
v  ǁVelocityǁ         0.00020852          25.885          7.7766          6.7789
v  Pressure                -507.49          206.21          28.743          31.682
v  k                   1.0056e-010          8.4301         0.15447         0.31068
v  omega                    57.492      2.732e+008     1.2912e+006           76891
v  TempK                    298.43          363.17          333.52          339.12
v  TurbVisc            2.5203e-018      0.00089196     3.7795e-005      0.00013284
v  CourantNb            0.00014815          1.5037         0.79624         0.97642
v  FourierNb             0.0037361               1         0.39759         0.12892
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035406     7.2983e-005      0.00019529

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.09          306.26
v  Yplus               0          2.9407         0.63512         0.49327


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67471            2.09          1.1938          1.1053


 INSTANT    0.500000000E-02   TIME STEP NUMBER             500
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925024E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16869E-01 0.46830E+01
   Friction velocity        uk    :  0.16869E-01 0.46790E+01
   Dimensionless distance   yplus :  0.11437E-01 0.29404E+01
   Friction thermal sca.    tstar :  0.10859E+01 0.15083E+03
   Rough dim-less th. sca.  tplus :  0.81023E-02 0.20830E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27899E+00       9   0.54817E-05   0.16608E+01 0.21274E+02 
c  Velocity[X]                                      0.72076E+00 
c  Velocity[Y]                                      0.44419E+00 
c  Velocity[Z]                                      0.49586E+00 
c  Pressure     0.11131E-04      16   0.19223E-03   0.10933E-01 0.18067E+02 
c  k            0.12001E-01      10   0.13638E-04   0.21731E-01 0.42350E+02 
c  omega        0.27922E+07       1   0.65928E-07   0.16940E+08 0.63815E+00 
c  TempK        0.10013E+05       6   0.32180E-05   0.21323E+02 0.16355E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6552e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.273      0.00014666       -0.012337
v  Velocity[Y]              -15.57          14.924         0.13853         0.19194
v  Velocity[Z]             -25.706          12.192         -1.6623        -0.50938
v  ǁVelocityǁ         0.00020461          25.881          7.7765          6.7787
v  Pressure                -507.87          206.11          28.643          31.584
v  k                   1.0055e-010          8.4276         0.15477         0.31143
v  omega                    57.491      2.732e+008     1.2912e+006           76892
v  TempK                    298.43          363.17          333.54          339.16
v  TurbVisc            2.5199e-018      0.00089463     3.7868e-005      0.00013311
v  CourantNb            0.00014832          1.5026         0.79622         0.97642
v  FourierNb             0.0037366               1         0.39765         0.12908
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035787     7.2984e-005      0.00019531

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.09          306.26
v  Yplus               0          2.9404         0.63512         0.49327


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41214           2.089          1.1939          1.1055


 INSTANT    0.501000000E-02   TIME STEP NUMBER             501
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925185E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16677E-01 0.46830E+01
   Friction velocity        uk    :  0.16677E-01 0.46790E+01
   Dimensionless distance   yplus :  0.11307E-01 0.29401E+01
   Friction thermal sca.    tstar :  0.10900E+01 0.15257E+03
   Rough dim-less th. sca.  tplus :  0.80100E-02 0.20828E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27901E+00       9   0.54866E-05   0.16730E+01 0.21379E+02 
c  Velocity[X]                                      0.72364E+00 
c  Velocity[Y]                                      0.45004E+00 
c  Velocity[Z]                                      0.49936E+00 
c  Pressure     0.10690E-04      17   0.19397E-03   0.10500E-01 0.19867E+02 
c  k            0.12034E-01      10   0.13689E-04   0.21771E-01 0.42281E+02 
c  omega        0.27922E+07       1   0.64517E-07   0.16772E+08 0.63910E+00 
c  TempK        0.10014E+05       6   0.32097E-05   0.21189E+02 0.16298E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6609e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.271     3.8908e-005       -0.012353
v  Velocity[Y]              -15.51           14.92         0.13889         0.19254
v  Velocity[Z]             -25.701          12.163         -1.6622        -0.50936
v  ǁVelocityǁ         0.00020099          25.876          7.7765          6.7785
v  Pressure                -508.27             206          28.529          31.472
v  k                   1.0053e-010          8.1196         0.15506         0.31218
v  omega                    57.491      2.732e+008     1.2912e+006           76892
v  TempK                    298.43          363.17          333.56           339.2
v  TurbVisc            2.5195e-018      0.00089765      3.794e-005      0.00013339
v  CourantNb            0.00014846          1.5013         0.79621         0.97641
v  FourierNb             0.0037371               1         0.39772         0.12923
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036174     7.2984e-005      0.00019533

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.09          306.27
v  Yplus               0          2.9401         0.63512         0.49326


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75862          2.0878          1.1939          1.1056


 INSTANT    0.502000000E-02   TIME STEP NUMBER             502
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924999E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16496E-01 0.46829E+01
   Friction velocity        uk    :  0.16496E-01 0.46789E+01
   Dimensionless distance   yplus :  0.11184E-01 0.29399E+01
   Friction thermal sca.    tstar :  0.10940E+01 0.15425E+03
   Rough dim-less th. sca.  tplus :  0.79230E-02 0.20826E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27903E+00       9   0.55005E-05   0.16622E+01 0.21306E+02 
c  Velocity[X]                                      0.72391E+00 
c  Velocity[Y]                                      0.44602E+00 
c  Velocity[Z]                                      0.49231E+00 
c  Pressure     0.10380E-04      17   0.18972E-03   0.10194E-01 0.18921E+02 
c  k            0.12068E-01      10   0.13724E-04   0.21823E-01 0.42197E+02 
c  omega        0.27922E+07       1   0.61054E-07   0.10737E+08 0.52400E+00 
c  TempK        0.10016E+05       6   0.32015E-05   0.21056E+02 0.16243E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6665e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253           19.27    -6.8002e-005       -0.012367
v  Velocity[Y]             -15.364          14.917         0.13925         0.19315
v  Velocity[Z]             -25.697          12.165         -1.6622        -0.50934
v  ǁVelocityǁ         0.00019742          25.872          7.7764          6.7783
v  Pressure                -508.68          205.89          28.421          31.368
v  k                   1.0051e-010          7.8712         0.15536         0.31293
v  omega                    57.491     2.7321e+008     1.2912e+006           76892
v  TempK                    298.43          363.17          333.58          339.24
v  TurbVisc            2.5191e-018       0.0009004     3.8012e-005      0.00013367
v  CourantNb            0.00014859             1.5         0.79619         0.97641
v  FourierNb             0.0037375               1         0.39778         0.12939
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036557     7.2985e-005      0.00019535

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.09          306.27
v  Yplus               0          2.9399         0.63511         0.49326


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66462          2.0866           1.194          1.1058


 INSTANT    0.503000000E-02   TIME STEP NUMBER             503
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925140E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16315E-01 0.46828E+01
   Friction velocity        uk    :  0.16315E-01 0.46789E+01
   Dimensionless distance   yplus :  0.11062E-01 0.29396E+01
   Friction thermal sca.    tstar :  0.10980E+01 0.15596E+03
   Rough dim-less th. sca.  tplus :  0.78361E-02 0.20824E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27904E+00       9   0.55138E-05   0.16645E+01 0.21292E+02 
c  Velocity[X]                                      0.72523E+00 
c  Velocity[Y]                                      0.44449E+00 
c  Velocity[Z]                                      0.49478E+00 
c  Pressure     0.10270E-04      17   0.18501E-03   0.10086E-01 0.18959E+02 
c  k            0.12101E-01      10   0.13693E-04   0.21971E-01 0.42227E+02 
c  omega        0.27922E+07       1   0.56824E-07   0.39609E+07 0.35675E+00 
c  TempK        0.10017E+05       6   0.31932E-05   0.20926E+02 0.16187E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6716e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.269     -0.00017532        -0.01238
v  Velocity[Y]             -15.288          14.913          0.1396         0.19375
v  Velocity[Z]             -25.693          12.167         -1.6621        -0.50933
v  ǁVelocityǁ         0.00019489          25.868          7.7763          6.7781
v  Pressure                -509.09          205.78          28.313          31.263
v  k                    1.005e-010          7.6559         0.15566         0.31367
v  omega                    57.491     2.7321e+008     1.2912e+006           76892
v  TempK                    298.43          363.17          333.61          339.28
v  TurbVisc            2.5187e-018      0.00090286     3.8085e-005      0.00013394
v  CourantNb            0.00014874          1.4989         0.79617         0.97641
v  FourierNb             0.0037379               1         0.39785         0.12955
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036934     7.2986e-005      0.00019538

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.1          306.27
v  Yplus               0          2.9396         0.63511         0.49326


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46641          2.0855           1.194           1.106


 INSTANT    0.504000000E-02   TIME STEP NUMBER             504
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925146E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16184E-01 0.46828E+01
   Friction velocity        uk    :  0.16184E-01 0.46788E+01
   Dimensionless distance   yplus :  0.10973E-01 0.29393E+01
   Friction thermal sca.    tstar :  0.11019E+01 0.15722E+03
   Rough dim-less th. sca.  tplus :  0.77732E-02 0.20823E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27906E+00       9   0.55214E-05   0.16691E+01 0.21320E+02 
c  Velocity[X]                                      0.72805E+00 
c  Velocity[Y]                                      0.44555E+00 
c  Velocity[Z]                                      0.49554E+00 
c  Pressure     0.10349E-04      16   0.18316E-03   0.10163E-01 0.18245E+02 
c  k            0.12134E-01      10   0.13725E-04   0.21952E-01 0.42113E+02 
c  omega        0.27922E+07       1   0.56573E-07   0.35166E+07 0.34624E+00 
c  TempK        0.10019E+05       6   0.31850E-05   0.20796E+02 0.16132E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.676e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.267     -0.00028108       -0.012393
v  Velocity[Y]             -15.282           14.91         0.13996         0.19436
v  Velocity[Z]             -25.689          12.169          -1.662        -0.50931
v  ǁVelocityǁ         0.00019158          25.864          7.7763          6.7779
v  Pressure                 -509.5          205.67          28.209          31.163
v  k                   1.0048e-010          7.3283         0.15595         0.31442
v  omega                    57.491     2.7321e+008     1.2912e+006           76892
v  TempK                    298.43          363.17          333.63          339.31
v  TurbVisc            2.5183e-018      0.00090505     3.8157e-005      0.00013422
v  CourantNb            0.00014881          1.4979         0.79616          0.9764
v  FourierNb             0.0037384               1         0.39791          0.1297
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037323     7.2987e-005       0.0001954

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.1          306.27
v  Yplus               0          2.9393         0.63511         0.49325


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76509          2.0846          1.1941          1.1061


 INSTANT    0.505000000E-02   TIME STEP NUMBER             505
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925146E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16011E-01 0.46827E+01
   Friction velocity        uk    :  0.16011E-01 0.46788E+01
   Dimensionless distance   yplus :  0.10856E-01 0.29391E+01
   Friction thermal sca.    tstar :  0.11059E+01 0.15892E+03
   Rough dim-less th. sca.  tplus :  0.76904E-02 0.20821E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27907E+00       9   0.55317E-05   0.16794E+01 0.21367E+02 
c  Velocity[X]                                      0.73147E+00 
c  Velocity[Y]                                      0.44698E+00 
c  Velocity[Z]                                      0.50097E+00 
c  Pressure     0.10849E-04      16   0.18457E-03   0.10654E-01 0.17381E+02 
c  k            0.12166E-01      10   0.13767E-04   0.22095E-01 0.42135E+02 
c  omega        0.27922E+07       1   0.58664E-07   0.63343E+07 0.41891E+00 
c  TempK        0.10020E+05       6   0.31768E-05   0.20669E+02 0.16077E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6797e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.265     -0.00038618       -0.012405
v  Velocity[Y]             -15.357          14.907         0.14031         0.19497
v  Velocity[Z]             -25.685          12.171          -1.662         -0.5093
v  ǁVelocityǁ         0.00018966          25.861          7.7762          6.7776
v  Pressure                -509.91          205.58          28.112           31.07
v  k                   1.0047e-010          7.3384         0.15625         0.31517
v  omega                    57.491     2.7321e+008     1.2912e+006           76893
v  TempK                    298.44          363.17          333.65          339.35
v  TurbVisc            2.5179e-018      0.00090697     3.8229e-005       0.0001345
v  CourantNb            0.00014895          1.4971         0.79614          0.9764
v  FourierNb              0.003739               1         0.39798         0.12986
v  total_pressure      1.0082e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037766     7.2989e-005      0.00019542

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.1          306.27
v  Yplus               0          2.9391         0.63511         0.49325


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.37358          2.0839          1.1941          1.1063


 INSTANT    0.506000000E-02   TIME STEP NUMBER             506
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925178E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15909E-01 0.46827E+01
   Friction velocity        uk    :  0.15909E-01 0.46787E+01
   Dimensionless distance   yplus :  0.10787E-01 0.29389E+01
   Friction thermal sca.    tstar :  0.11098E+01 0.15994E+03
   Rough dim-less th. sca.  tplus :  0.76413E-02 0.20819E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27909E+00       9   0.55514E-05   0.16930E+01 0.21453E+02 
c  Velocity[X]                                      0.73572E+00 
c  Velocity[Y]                                      0.45035E+00 
c  Velocity[Z]                                      0.50695E+00 
c  Pressure     0.10828E-04      17   0.18769E-03   0.10633E-01 0.16537E+02 
c  k            0.12199E-01      10   0.13850E-04   0.22333E-01 0.42207E+02 
c  omega        0.27922E+07       1   0.62895E-07   0.13481E+08 0.57562E+00 
c  TempK        0.10021E+05       6   0.31687E-05   0.20543E+02 0.16022E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.683e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.264      -0.0004872       -0.012416
v  Velocity[Y]             -15.405          14.905         0.14065         0.19557
v  Velocity[Z]             -25.682          12.173         -1.6619        -0.50929
v  ǁVelocityǁ         0.00018729          25.857          7.7761          6.7774
v  Pressure                -510.32          205.48          28.021          30.981
v  k                   1.0045e-010          7.3489         0.15654         0.31592
v  omega                    57.491     2.7321e+008     1.2912e+006           76893
v  TempK                    298.44          363.17          333.67          339.39
v  TurbVisc            2.5175e-018      0.00090861     3.8302e-005      0.00013477
v  CourantNb              0.000149          1.4963         0.79613         0.97639
v  FourierNb             0.0037396               1         0.39804         0.13002
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038286     7.2991e-005      0.00019544

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.1          306.27
v  Yplus               0          2.9389         0.63511         0.49324


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5562          2.0832          1.1942          1.1064


 INSTANT    0.507000000E-02   TIME STEP NUMBER             507
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925093E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15783E-01 0.46827E+01
   Friction velocity        uk    :  0.15783E-01 0.46787E+01
   Dimensionless distance   yplus :  0.10701E-01 0.29387E+01
   Friction thermal sca.    tstar :  0.11137E+01 0.16122E+03
   Rough dim-less th. sca.  tplus :  0.75807E-02 0.20818E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27910E+00       9   0.55715E-05   0.16988E+01 0.21558E+02 
c  Velocity[X]                                      0.73970E+00 
c  Velocity[Y]                                      0.45849E+00 
c  Velocity[Z]                                      0.50063E+00 
c  Pressure     0.10750E-04      17   0.19126E-03   0.10555E-01 0.16039E+02 
c  k            0.12232E-01      10   0.13865E-04   0.22331E-01 0.42058E+02 
c  omega        0.27922E+07       1   0.66262E-07   0.18951E+08 0.67397E+00 
c  TempK        0.10023E+05       6   0.31605E-05   0.20419E+02 0.15968E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.687e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.262     -0.00058795       -0.012426
v  Velocity[Y]             -15.316          14.902           0.141         0.19618
v  Velocity[Z]             -25.678          12.175         -1.6619        -0.50928
v  ǁVelocityǁ         0.00018482          25.853           7.776          6.7772
v  Pressure                -510.74          205.39          27.933          30.897
v  k                   1.0043e-010          7.3598         0.15684         0.31667
v  omega                    57.491     2.7321e+008     1.2912e+006           76893
v  TempK                    298.44          363.17           333.7          339.43
v  TurbVisc            2.5171e-018      0.00090999     3.8374e-005      0.00013505
v  CourantNb            0.00014909          1.4954         0.79611         0.97639
v  FourierNb             0.0037401               1         0.39811         0.13018
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038891     7.2993e-005      0.00019547

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.1          306.27
v  Yplus               0          2.9387         0.63511         0.49323


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69298          2.0824          1.1942          1.1066


 INSTANT    0.508000000E-02   TIME STEP NUMBER             508
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925034E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15649E-01 0.46826E+01
   Friction velocity        uk    :  0.15648E-01 0.46786E+01
   Dimensionless distance   yplus :  0.10610E-01 0.29384E+01
   Friction thermal sca.    tstar :  0.11175E+01 0.16260E+03
   Rough dim-less th. sca.  tplus :  0.75161E-02 0.20816E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27911E+00       9   0.55894E-05   0.17007E+01 0.21537E+02 
c  Velocity[X]                                      0.74301E+00 
c  Velocity[Y]                                      0.45560E+00 
c  Velocity[Z]                                      0.50208E+00 
c  Pressure     0.11918E-04      17   0.19124E-03   0.11700E-01 0.16257E+02 
c  k            0.12264E-01      10   0.13953E-04   0.22327E-01 0.41868E+02 
c  omega        0.27922E+07       1   0.58879E-07   0.64714E+07 0.42663E+00 
c  TempK        0.10024E+05       6   0.31524E-05   0.20297E+02 0.15915E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6907e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253           19.26     -0.00068759       -0.012437
v  Velocity[Y]             -15.218            14.9         0.14134         0.19679
v  Velocity[Z]             -25.674          12.176         -1.6618        -0.50926
v  ǁVelocityǁ         0.00018254           25.85          7.7759          6.7769
v  Pressure                -511.18           205.3          27.844          30.811
v  k                   1.0042e-010           7.371         0.15713         0.31742
v  omega                    57.491     2.7321e+008     1.2912e+006           76893
v  TempK                    298.44          363.17          333.72          339.46
v  TurbVisc            2.5167e-018      0.00091241     3.8447e-005      0.00013533
v  CourantNb             0.0001492          1.4946         0.79609         0.97639
v  FourierNb             0.0037402               1         0.39817         0.13034
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039625     7.2996e-005      0.00019549

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.11          306.28
v  Yplus               0          2.9384          0.6351         0.49323


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56238          2.0816          1.1943          1.1067


 INSTANT    0.509000000E-02   TIME STEP NUMBER             509
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925160E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15524E-01 0.46826E+01
   Friction velocity        uk    :  0.15524E-01 0.46786E+01
   Dimensionless distance   yplus :  0.10526E-01 0.29381E+01
   Friction thermal sca.    tstar :  0.11214E+01 0.16391E+03
   Rough dim-less th. sca.  tplus :  0.74564E-02 0.20814E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27912E+00       9   0.56103E-05   0.17051E+01 0.21546E+02 
c  Velocity[X]                                      0.74473E+00 
c  Velocity[Y]                                      0.45655E+00 
c  Velocity[Z]                                      0.50379E+00 
c  Pressure     0.11299E-04      17   0.19199E-03   0.11093E-01 0.17137E+02 
c  k            0.12297E-01      10   0.14064E-04   0.22375E-01 0.41723E+02 
c  omega        0.27922E+07       1   0.59441E-07   0.78356E+07 0.46435E+00 
c  TempK        0.10026E+05       6   0.31444E-05   0.20180E+02 0.15862E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6937e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.258     -0.00078371       -0.012447
v  Velocity[Y]             -15.172          14.898         0.14168         0.19741
v  Velocity[Z]              -25.67          12.178         -1.6618        -0.50925
v  ǁVelocityǁ         0.00018142          25.846          7.7758          6.7767
v  Pressure                -511.63           205.2          27.747          30.718
v  k                    1.004e-010          7.3826         0.15743         0.31816
v  omega                     57.49     2.7321e+008     1.2912e+006           76894
v  TempK                    298.44          363.17          333.74           339.5
v  TurbVisc            2.5163e-018      0.00091461     3.8519e-005       0.0001356
v  CourantNb             0.0001493          1.4939         0.79608         0.97638
v  FourierNb             0.0037402               1         0.39824          0.1305
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.003996     7.2998e-005      0.00019552

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.11          306.28
v  Yplus               0          2.9381         0.63509         0.49322


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81212           2.081          1.1943          1.1069


 INSTANT    0.510000000E-02   TIME STEP NUMBER             510
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925136E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15462E-01 0.46825E+01
   Friction velocity        uk    :  0.15462E-01 0.46786E+01
   Dimensionless distance   yplus :  0.10484E-01 0.29379E+01
   Friction thermal sca.    tstar :  0.11252E+01 0.16457E+03
   Rough dim-less th. sca.  tplus :  0.74266E-02 0.20812E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27913E+00       9   0.56385E-05   0.17120E+01 0.21563E+02 
c  Velocity[X]                                      0.74778E+00 
c  Velocity[Y]                                      0.45711E+00 
c  Velocity[Z]                                      0.50709E+00 
c  Pressure     0.10931E-04      17   0.19562E-03   0.10731E-01 0.16446E+02 
c  k            0.12329E-01      10   0.14155E-04   0.22477E-01 0.41638E+02 
c  omega        0.27922E+07       1   0.57092E-07   0.35741E+07 0.34401E+00 
c  TempK        0.10027E+05       6   0.31363E-05   0.20064E+02 0.15810E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.696e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.256     -0.00087944       -0.012455
v  Velocity[Y]             -15.171          14.897         0.14202         0.19802
v  Velocity[Z]             -25.667           12.18         -1.6617        -0.50924
v  ǁVelocityǁ         0.00017922          25.842          7.7757          6.7764
v  Pressure                -512.08          205.11          27.656          30.631
v  k                   1.0039e-010          7.3945         0.15772         0.31891
v  omega                    57.491     2.7321e+008     1.2912e+006           76894
v  TempK                    298.44          363.17          333.76          339.54
v  TurbVisc             2.516e-018      0.00091652     3.8592e-005      0.00013588
v  CourantNb            0.00014933          1.4934         0.79606         0.97638
v  FourierNb             0.0037403               1          0.3983         0.13066
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039973     7.3001e-005      0.00019554

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.11          306.28
v  Yplus               0          2.9379         0.63509         0.49321


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56318          2.0806          1.1944           1.107


 INSTANT    0.511000000E-02   TIME STEP NUMBER             511
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925035E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15339E-01 0.46825E+01
   Friction velocity        uk    :  0.15339E-01 0.46785E+01
   Dimensionless distance   yplus :  0.10400E-01 0.29377E+01
   Friction thermal sca.    tstar :  0.11290E+01 0.16589E+03
   Rough dim-less th. sca.  tplus :  0.73673E-02 0.20811E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27914E+00       9   0.56620E-05   0.17209E+01 0.21624E+02 
c  Velocity[X]                                      0.75089E+00 
c  Velocity[Y]                                      0.45887E+00 
c  Velocity[Z]                                      0.51119E+00 
c  Pressure     0.10952E-04      17   0.19284E-03   0.10751E-01 0.14787E+02 
c  k            0.12362E-01      10   0.14255E-04   0.22634E-01 0.41614E+02 
c  omega        0.27922E+07       1   0.59144E-07   0.64794E+07 0.42522E+00 
c  TempK        0.10028E+05       6   0.31283E-05   0.19948E+02 0.15759E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6975e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.253     -0.00097283       -0.012463
v  Velocity[Y]             -15.241          14.895         0.14235         0.19863
v  Velocity[Z]             -25.664          12.182         -1.6617        -0.50923
v  ǁVelocityǁ         0.00017857          25.839          7.7756          6.7761
v  Pressure                -512.52          205.03          27.576          30.554
v  k                   1.0037e-010          7.4068         0.15802         0.31967
v  omega                    57.491     2.7321e+008     1.2912e+006           76894
v  TempK                    298.44          363.17          333.78          339.58
v  TurbVisc            2.5156e-018      0.00091815     3.8664e-005      0.00013616
v  CourantNb            0.00014944          1.4931         0.79605         0.97638
v  FourierNb             0.0037405               1         0.39837         0.13082
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.003983     7.3002e-005      0.00019556

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.11          306.28
v  Yplus               0          2.9377         0.63509          0.4932


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70479          2.0804          1.1944          1.1072


 INSTANT    0.512000000E-02   TIME STEP NUMBER             512
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925082E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15302E-01 0.46825E+01
   Friction velocity        uk    :  0.15302E-01 0.46785E+01
   Dimensionless distance   yplus :  0.10375E-01 0.29375E+01
   Friction thermal sca.    tstar :  0.11328E+01 0.16629E+03
   Rough dim-less th. sca.  tplus :  0.73496E-02 0.20809E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27915E+00       9   0.56877E-05   0.17328E+01 0.21697E+02 
c  Velocity[X]                                      0.75521E+00 
c  Velocity[Y]                                      0.46279E+00 
c  Velocity[Z]                                      0.51482E+00 
c  Pressure     0.11054E-04      16   0.19370E-03   0.10851E-01 0.14300E+02 
c  k            0.12394E-01      10   0.14365E-04   0.22807E-01 0.41594E+02 
c  omega        0.27922E+07       1   0.66615E-07   0.20760E+08 0.70304E+00 
c  TempK        0.10030E+05       6   0.31202E-05   0.19832E+02 0.15708E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6988e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.251       -0.001064        -0.01247
v  Velocity[Y]             -15.295          14.894         0.14267         0.19925
v  Velocity[Z]             -25.661          12.184         -1.6616        -0.50922
v  ǁVelocityǁ         0.00017735          25.836          7.7755          6.7758
v  Pressure                -512.96          204.95          27.499          30.481
v  k                   1.0036e-010          7.4193         0.15831         0.32042
v  omega                    57.491     2.7321e+008     1.2912e+006           76894
v  TempK                    298.44          363.17           333.8          339.61
v  TurbVisc            2.5152e-018      0.00091951     3.8737e-005      0.00013643
v  CourantNb            0.00014944          1.4928         0.79603         0.97637
v  FourierNb             0.0037408               1         0.39844         0.13098
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039611     7.3003e-005      0.00019559

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.11          306.28
v  Yplus               0          2.9375         0.63509         0.49319


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49462          2.0802          1.1945          1.1074


 INSTANT    0.513000000E-02   TIME STEP NUMBER             513
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925226E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15233E-01 0.46824E+01
   Friction velocity        uk    :  0.15233E-01 0.46785E+01
   Dimensionless distance   yplus :  0.10328E-01 0.29373E+01
   Friction thermal sca.    tstar :  0.11366E+01 0.16705E+03
   Rough dim-less th. sca.  tplus :  0.73164E-02 0.20808E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27916E+00       9   0.57159E-05   0.17436E+01 0.21761E+02 
c  Velocity[X]                                      0.75882E+00 
c  Velocity[Y]                                      0.46719E+00 
c  Velocity[Z]                                      0.51758E+00 
c  Pressure     0.11125E-04      17   0.19609E-03   0.10920E-01 0.14938E+02 
c  k            0.12426E-01      10   0.14441E-04   0.22933E-01 0.41512E+02 
c  omega        0.27922E+07       1   0.62480E-07   0.12460E+08 0.56006E+00 
c  TempK        0.10031E+05       6   0.31122E-05   0.19716E+02 0.15657E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7006e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.249      -0.0011553       -0.012478
v  Velocity[Y]             -15.217          14.893           0.143         0.19986
v  Velocity[Z]             -25.658          12.186         -1.6616        -0.50921
v  ǁVelocityǁ         0.00017661          25.833          7.7754          6.7755
v  Pressure                -513.42          204.86          27.417          30.403
v  k                   1.0034e-010          7.4321         0.15861         0.32117
v  omega                    57.491     2.7321e+008     1.2912e+006           76894
v  TempK                    298.44          363.17          333.83          339.65
v  TurbVisc            2.5148e-018       0.0009206      3.881e-005      0.00013671
v  CourantNb            0.00014948          1.4924         0.79602         0.97637
v  FourierNb             0.0037414               1          0.3985         0.13114
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039337     7.3005e-005      0.00019561

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.12          306.28
v  Yplus               0          2.9373         0.63508         0.49318


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35489          2.0798          1.1945          1.1075


 INSTANT    0.514000000E-02   TIME STEP NUMBER             514
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925064E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15190E-01 0.46824E+01
   Friction velocity        uk    :  0.15190E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10299E-01 0.29371E+01
   Friction thermal sca.    tstar :  0.11396E+01 0.16752E+03
   Rough dim-less th. sca.  tplus :  0.72961E-02 0.20806E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27917E+00       9   0.57513E-05   0.17464E+01 0.21774E+02 
c  Velocity[X]                                      0.76229E+00 
c  Velocity[Y]                                      0.46564E+00 
c  Velocity[Z]                                      0.51843E+00 
c  Pressure     0.11219E-04      16   0.20613E-03   0.11012E-01 0.12912E+02 
c  k            0.12458E-01      10   0.14551E-04   0.23094E-01 0.41501E+02 
c  omega        0.27922E+07       1   0.61344E-07   0.93025E+07 0.49269E+00 
c  TempK        0.10032E+05       6   0.31041E-05   0.19599E+02 0.15607E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7022e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.246      -0.0012463       -0.012484
v  Velocity[Y]             -15.165          14.892         0.14332         0.20048
v  Velocity[Z]             -25.654          12.187         -1.6616         -0.5092
v  ǁVelocityǁ         0.00017525           25.83          7.7753          6.7752
v  Pressure                -513.87           204.8          27.352          30.342
v  k                   1.0033e-010           7.445         0.15891         0.32192
v  omega                    57.491     2.7321e+008     1.2912e+006           76895
v  TempK                    298.44          363.17          333.85          339.69
v  TurbVisc            2.5144e-018      0.00092143     3.8883e-005      0.00013699
v  CourantNb            0.00014951           1.492           0.796         0.97636
v  FourierNb              0.003742               1         0.39857         0.13131
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034874     7.3007e-005      0.00019563

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.12          306.28
v  Yplus               0          2.9371         0.63508         0.49318


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55129          2.0795          1.1946          1.1077


 INSTANT    0.515000000E-02   TIME STEP NUMBER             515
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925261E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15113E-01 0.46824E+01
   Friction velocity        uk    :  0.15113E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10247E-01 0.29368E+01
   Friction thermal sca.    tstar :  0.11416E+01 0.16838E+03
   Rough dim-less th. sca.  tplus :  0.72588E-02 0.20805E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27917E+00       9   0.57903E-05   0.17594E+01 0.21870E+02 
c  Velocity[X]                                      0.76827E+00 
c  Velocity[Y]                                      0.47055E+00 
c  Velocity[Z]                                      0.52063E+00 
c  Pressure     0.11543E-04      16   0.25096E-03   0.11330E-01 0.14168E+02 
c  k            0.12490E-01      10   0.14661E-04   0.23308E-01 0.41542E+02 
c  omega        0.27922E+07       1   0.59871E-07   0.75583E+07 0.45495E+00 
c  TempK        0.10033E+05       6   0.30960E-05   0.19483E+02 0.15556E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7033e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.244      -0.0013356        -0.01249
v  Velocity[Y]             -15.172          14.891         0.14364          0.2011
v  Velocity[Z]             -25.651          12.189         -1.6615         -0.5092
v  ǁVelocityǁ         0.00017517          25.827          7.7752          6.7749
v  Pressure                -514.33          204.72          27.275          30.269
v  k                   1.0031e-010          7.4581          0.1592         0.32268
v  omega                    57.491     2.7321e+008     1.2912e+006           76895
v  TempK                    298.44          363.17          333.87          339.72
v  TurbVisc             2.514e-018      0.00092199     3.8956e-005      0.00013727
v  CourantNb            0.00014958          1.4918         0.79598         0.97636
v  FourierNb             0.0037426               1         0.39863         0.13147
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0030668     7.3008e-005      0.00019565

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.12          306.29
v  Yplus               0          2.9368         0.63507         0.49317


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75343          2.0794          1.1946          1.1078


 INSTANT    0.516000000E-02   TIME STEP NUMBER             516
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925223E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15107E-01 0.46824E+01
   Friction velocity        uk    :  0.15107E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10243E-01 0.29366E+01
   Friction thermal sca.    tstar :  0.11436E+01 0.16844E+03
   Rough dim-less th. sca.  tplus :  0.72561E-02 0.20803E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27918E+00       9   0.58148E-05   0.17662E+01 0.21879E+02 
c  Velocity[X]                                      0.77262E+00 
c  Velocity[Y]                                      0.46925E+00 
c  Velocity[Z]                                      0.52435E+00 
c  Pressure     0.11351E-04      17   0.25728E-03   0.11142E-01 0.13277E+02 
c  k            0.12522E-01      10   0.14803E-04   0.23446E-01 0.41502E+02 
c  omega        0.27922E+07       1   0.62321E-07   0.10935E+08 0.52783E+00 
c  TempK        0.10035E+05       6   0.30879E-05   0.19367E+02 0.15505E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7038e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.241      -0.0014257       -0.012496
v  Velocity[Y]             -15.278          14.891         0.14395         0.20172
v  Velocity[Z]             -25.648          12.191         -1.6615        -0.50919
v  ǁVelocityǁ         0.00017435          25.823          7.7751          6.7746
v  Pressure                -514.79          204.65          27.206          30.203
v  k                    1.003e-010          7.4713          0.1595         0.32343
v  omega                    57.491     2.7321e+008     1.2912e+006           76895
v  TempK                    298.44          363.17          333.89          339.76
v  TurbVisc            2.5136e-018      0.00092232     3.9029e-005      0.00013755
v  CourantNb            0.00014956          1.4917         0.79597         0.97635
v  FourierNb              0.003743               1          0.3987         0.13164
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0032484     7.3011e-005      0.00019568

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.12          306.29
v  Yplus               0          2.9366         0.63507         0.49316


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68892          2.0794          1.1947           1.108


 INSTANT    0.517000000E-02   TIME STEP NUMBER             517
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925237E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15061E-01 0.46824E+01
   Friction velocity        uk    :  0.15061E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10211E-01 0.29364E+01
   Friction thermal sca.    tstar :  0.11456E+01 0.16896E+03
   Rough dim-less th. sca.  tplus :  0.72338E-02 0.20801E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27918E+00       9   0.58329E-05   0.17753E+01 0.21934E+02 
c  Velocity[X]                                      0.77706E+00 
c  Velocity[Y]                                      0.47149E+00 
c  Velocity[Z]                                      0.52673E+00 
c  Pressure     0.11074E-04      16   0.21879E-03   0.10869E-01 0.12398E+02 
c  k            0.12554E-01      10   0.14916E-04   0.23665E-01 0.41531E+02 
c  omega        0.27922E+07       1   0.63166E-07   0.14456E+08 0.59387E+00 
c  TempK        0.10036E+05       6   0.30799E-05   0.19251E+02 0.15455E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7039e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.238      -0.0015132       -0.012502
v  Velocity[Y]             -15.351           14.89         0.14425         0.20233
v  Velocity[Z]             -25.645          12.192         -1.6615        -0.50918
v  ǁVelocityǁ         0.00017458           25.82          7.7749          6.7743
v  Pressure                -515.23          204.58          27.142          30.143
v  k                   1.0028e-010          7.4846          0.1598         0.32419
v  omega                    57.491     2.7321e+008     1.2912e+006           76895
v  TempK                    298.44          363.17          333.91          339.79
v  TurbVisc            2.5133e-018      0.00092239     3.9102e-005      0.00013782
v  CourantNb            0.00014959          1.4917         0.79595         0.97635
v  FourierNb              0.003743               1         0.39876          0.1318
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0033468     7.3013e-005       0.0001957

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.12          306.29
v  Yplus               0          2.9364         0.63507         0.49315


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49757          2.0794          1.1947          1.1082


 INSTANT    0.518000000E-02   TIME STEP NUMBER             518
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925247E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15073E-01 0.46824E+01
   Friction velocity        uk    :  0.15073E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10220E-01 0.29362E+01
   Friction thermal sca.    tstar :  0.11476E+01 0.16882E+03
   Rough dim-less th. sca.  tplus :  0.72399E-02 0.20800E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27919E+00       9   0.58605E-05   0.17863E+01 0.21978E+02 
c  Velocity[X]                                      0.78132E+00 
c  Velocity[Y]                                      0.47431E+00 
c  Velocity[Z]                                      0.53067E+00 
c  Pressure     0.11311E-04      17   0.21256E-03   0.11102E-01 0.12454E+02 
c  k            0.12585E-01      10   0.15084E-04   0.23871E-01 0.41543E+02 
c  omega        0.27922E+07       1   0.60614E-07   0.93587E+07 0.49593E+00 
c  TempK        0.10037E+05       6   0.30718E-05   0.19136E+02 0.15404E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7046e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.235      -0.0016033       -0.012507
v  Velocity[Y]             -15.304          14.889         0.14456         0.20295
v  Velocity[Z]             -25.642          12.194         -1.6614        -0.50917
v  ǁVelocityǁ         0.00017384          25.817          7.7748           6.774
v  Pressure                -515.68          204.52          27.078          30.084
v  k                   1.0026e-010          7.4978          0.1601         0.32494
v  omega                    57.491     2.7321e+008     1.2912e+006           76895
v  TempK                    298.44          363.17          333.93          339.83
v  TurbVisc            2.5129e-018      0.00092222     3.9176e-005       0.0001381
v  CourantNb            0.00014956          1.4915         0.79594         0.97634
v  FourierNb              0.003743               1         0.39883         0.13197
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.003375     7.3014e-005      0.00019572

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.13          306.29
v  Yplus               0          2.9362         0.63506         0.49314


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54387          2.0793          1.1948          1.1083


 INSTANT    0.519000000E-02   TIME STEP NUMBER             519
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925249E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15031E-01 0.46824E+01
   Friction velocity        uk    :  0.15031E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10191E-01 0.29360E+01
   Friction thermal sca.    tstar :  0.11496E+01 0.16930E+03
   Rough dim-less th. sca.  tplus :  0.72195E-02 0.20799E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27919E+00       9   0.58773E-05   0.17904E+01 0.21957E+02 
c  Velocity[X]                                      0.78399E+00 
c  Velocity[Y]                                      0.47172E+00 
c  Velocity[Z]                                      0.53466E+00 
c  Pressure     0.11160E-04      17   0.20388E-03   0.10953E-01 0.12099E+02 
c  k            0.12617E-01      11   0.14486E-04   0.24117E-01 0.41587E+02 
c  omega        0.27922E+07       1   0.57236E-07   0.34902E+07 0.33718E+00 
c  TempK        0.10038E+05       6   0.30637E-05   0.19022E+02 0.15354E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7052e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.232      -0.0016928       -0.012513
v  Velocity[Y]             -15.272          14.889         0.14485         0.20358
v  Velocity[Z]             -25.639          12.195         -1.6614        -0.50916
v  ǁVelocityǁ          0.0001739          25.815          7.7747          6.7736
v  Pressure                -516.13          204.45          27.016          30.027
v  k                   1.0025e-010           7.511          0.1604          0.3257
v  omega                    57.491     2.7321e+008     1.2912e+006           76896
v  TempK                    298.44          363.17          333.95          339.87
v  TurbVisc            2.5125e-018      0.00092182     3.9249e-005      0.00013838
v  CourantNb             0.0001496          1.4914         0.79592         0.97634
v  FourierNb             0.0037432               1         0.39889         0.13213
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034008     7.3016e-005      0.00019575

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.13          306.29
v  Yplus               0           2.936         0.63506         0.49312


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74484          2.0793          1.1948          1.1085


 INSTANT    0.520000000E-02   TIME STEP NUMBER             520
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925250E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15034E-01 0.46823E+01
   Friction velocity        uk    :  0.15034E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10193E-01 0.29358E+01
   Friction thermal sca.    tstar :  0.11516E+01 0.16927E+03
   Rough dim-less th. sca.  tplus :  0.72210E-02 0.20797E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27919E+00       9   0.58895E-05   0.17933E+01 0.21995E+02 
c  Velocity[X]                                      0.78690E+00 
c  Velocity[Y]                                      0.47318E+00 
c  Velocity[Z]                                      0.53322E+00 
c  Pressure     0.10926E-04      17   0.19971E-03   0.10723E-01 0.11809E+02 
c  k            0.12649E-01      11   0.14613E-04   0.24361E-01 0.41616E+02 
c  omega        0.27922E+07       1   0.58559E-07   0.55544E+07 0.39827E+00 
c  TempK        0.10039E+05       6   0.30556E-05   0.18910E+02 0.15305E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7055e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.229      -0.0017839       -0.012518
v  Velocity[Y]             -15.291          14.889         0.14515          0.2042
v  Velocity[Z]             -25.636          12.197         -1.6614        -0.50916
v  ǁVelocityǁ         0.00017373          25.812          7.7745          6.7733
v  Pressure                -516.58          204.39          26.956          29.971
v  k                   1.0023e-010          7.5241          0.1607         0.32646
v  omega                    57.491     2.7321e+008     1.2912e+006           76896
v  TempK                    298.45          363.17          333.97           339.9
v  TurbVisc            2.5121e-018      0.00092119     3.9323e-005      0.00013866
v  CourantNb            0.00014959          1.4913         0.79591         0.97633
v  FourierNb             0.0037435               1         0.39896          0.1323
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0034302     7.3017e-005      0.00019577

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.13          306.29
v  Yplus               0          2.9358         0.63506         0.49311


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76784          2.0793          1.1949          1.1086


 INSTANT    0.521000000E-02   TIME STEP NUMBER             521
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925293E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15024E-01 0.46823E+01
   Friction velocity        uk    :  0.15024E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10187E-01 0.29356E+01
   Friction thermal sca.    tstar :  0.11535E+01 0.16938E+03
   Rough dim-less th. sca.  tplus :  0.72162E-02 0.20796E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27920E+00       9   0.59103E-05   0.18085E+01 0.22102E+02 
c  Velocity[X]                                      0.79144E+00 
c  Velocity[Y]                                      0.47771E+00 
c  Velocity[Z]                                      0.53935E+00 
c  Pressure     0.11239E-04      16   0.19869E-03   0.11031E-01 0.10961E+02 
c  k            0.12680E-01      11   0.14737E-04   0.24519E-01 0.41550E+02 
c  omega        0.27922E+07       1   0.62901E-07   0.11383E+08 0.53785E+00 
c  TempK        0.10041E+05       6   0.30475E-05   0.18800E+02 0.15256E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7053e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.226      -0.0018733       -0.012522
v  Velocity[Y]             -15.404          14.889         0.14545         0.20482
v  Velocity[Z]             -25.634          12.198         -1.6614        -0.50915
v  ǁVelocityǁ         0.00017424          25.809          7.7744          6.7729
v  Pressure                -517.01          204.34          26.906          29.924
v  k                   1.0022e-010          7.5369           0.161         0.32721
v  omega                    57.491     2.7321e+008     1.2912e+006           76896
v  TempK                    298.45          363.17          333.99          339.94
v  TurbVisc            2.5117e-018      0.00092035     3.9397e-005      0.00013894
v  CourantNb            0.00014959          1.4914         0.79589         0.97633
v  FourierNb             0.0037439               1         0.39902         0.13247
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0034643     7.3018e-005      0.00019579

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.13          306.29
v  Yplus               0          2.9356         0.63505          0.4931


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52261          2.0794          1.1949          1.1088


 INSTANT    0.522000000E-02   TIME STEP NUMBER             522
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925332E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15054E-01 0.46823E+01
   Friction velocity        uk    :  0.15054E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10207E-01 0.29353E+01
   Friction thermal sca.    tstar :  0.11555E+01 0.16905E+03
   Rough dim-less th. sca.  tplus :  0.72304E-02 0.20794E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27920E+00       9   0.59325E-05   0.18232E+01 0.22199E+02 
c  Velocity[X]                                      0.79773E+00 
c  Velocity[Y]                                      0.48213E+00 
c  Velocity[Z]                                      0.54338E+00 
c  Pressure     0.11202E-04      15   0.20097E-03   0.10995E-01 0.11283E+02 
c  k            0.12712E-01      11   0.14937E-04   0.24755E-01 0.41570E+02 
c  omega        0.27922E+07       1   0.65499E-07   0.18081E+08 0.66098E+00 
c  TempK        0.10042E+05       6   0.30394E-05   0.18690E+02 0.15207E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7049e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.254          19.223      -0.0019592       -0.012527
v  Velocity[Y]             -15.479          14.889         0.14574         0.20544
v  Velocity[Z]             -25.631            12.2         -1.6613        -0.50914
v  ǁVelocityǁ         0.00017468          25.806          7.7742          6.7725
v  Pressure                -517.44          204.28          26.851          29.873
v  k                   1.0021e-010          7.5495          0.1613         0.32797
v  omega                     57.49     2.7321e+008     1.2912e+006           76896
v  TempK                    298.45          363.17          334.02          339.97
v  TurbVisc            2.5114e-018       0.0009193     3.9471e-005      0.00013922
v  CourantNb            0.00014955          1.4915         0.79588         0.97632
v  FourierNb             0.0037444               1         0.39909         0.13264
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0034997      7.302e-005      0.00019582

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.13          306.29
v  Yplus               0          2.9353         0.63505         0.49309


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61553          2.0796           1.195           1.109


 INSTANT    0.523000000E-02   TIME STEP NUMBER             523
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925492E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15080E-01 0.46823E+01
   Friction velocity        uk    :  0.15079E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10224E-01 0.29351E+01
   Friction thermal sca.    tstar :  0.11575E+01 0.16876E+03
   Rough dim-less th. sca.  tplus :  0.72428E-02 0.20793E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27920E+00       9   0.59606E-05   0.18303E+01 0.22232E+02 
c  Velocity[X]                                      0.80315E+00 
c  Velocity[Y]                                      0.48499E+00 
c  Velocity[Z]                                      0.54219E+00 
c  Pressure     0.11201E-04      16   0.19963E-03   0.10994E-01 0.11982E+02 
c  k            0.12743E-01      11   0.15059E-04   0.24940E-01 0.41569E+02 
c  omega        0.27922E+07       1   0.62883E-07   0.13093E+08 0.57326E+00 
c  TempK        0.10043E+05       6   0.30313E-05   0.18579E+02 0.15157E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7051e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.254           19.22      -0.0020462        -0.01253
v  Velocity[Y]             -15.434          14.889         0.14603         0.20607
v  Velocity[Z]             -25.628          12.201         -1.6613        -0.50912
v  ǁVelocityǁ         0.00017508          25.803           7.774          6.7722
v  Pressure                -517.87          204.22          26.791          29.817
v  k                   1.0019e-010          7.5618          0.1616         0.32873
v  omega                     57.49     2.7321e+008     1.2912e+006           76896
v  TempK                    298.45          363.17          334.04          340.01
v  TurbVisc             2.511e-018      0.00091804     3.9545e-005       0.0001395
v  CourantNb            0.00014952          1.4914         0.79586         0.97631
v  FourierNb              0.003745               1         0.39915         0.13281
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0036354     7.3022e-005      0.00019585

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.14           306.3
v  Yplus               0          2.9351         0.63505         0.49308


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61033          2.0796           1.195          1.1091


 INSTANT    0.524000000E-02   TIME STEP NUMBER             524
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925229E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15101E-01 0.46823E+01
   Friction velocity        uk    :  0.15101E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10239E-01 0.29349E+01
   Friction thermal sca.    tstar :  0.11594E+01 0.27287E+03
   Rough dim-less th. sca.  tplus :  0.72533E-02 0.20791E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27920E+00       9   0.59868E-05   0.18327E+01 0.22204E+02 
c  Velocity[X]                                      0.80796E+00 
c  Velocity[Y]                                      0.48123E+00 
c  Velocity[Z]                                      0.54356E+00 
c  Pressure     0.11044E-04      15   0.19666E-03   0.10840E-01 0.10208E+02 
c  k            0.12774E-01      11   0.15161E-04   0.25174E-01 0.41628E+02 
c  omega        0.27922E+07       1   0.57707E-07   0.36632E+07 0.34334E+00 
c  TempK        0.10044E+05       6   0.30233E-05   0.18469E+02 0.15108E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7054e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.254          19.217      -0.0021321       -0.012532
v  Velocity[Y]             -15.403          14.889         0.14632          0.2067
v  Velocity[Z]             -25.625          12.202         -1.6613        -0.50911
v  ǁVelocityǁ          0.0001756          25.801          7.7739          6.7718
v  Pressure                -518.29          204.17          26.745          29.776
v  k                   1.0018e-010          7.5737          0.1619         0.32949
v  omega                     57.49     2.7321e+008     1.2912e+006           76896
v  TempK                    298.45          363.17          334.06          340.04
v  TurbVisc            2.5106e-018      0.00091631     3.9619e-005      0.00013978
v  CourantNb             0.0001495          1.4913         0.79585         0.97631
v  FourierNb             0.0037454               1         0.39922         0.13298
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0036671     7.3025e-005      0.00019587

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.14           306.3
v  Yplus               0          2.9349         0.63504         0.49306


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71836          2.0796          1.1951          1.1093


 INSTANT    0.525000000E-02   TIME STEP NUMBER             525
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925611E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15132E-01 0.46823E+01
   Friction velocity        uk    :  0.15132E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10260E-01 0.29347E+01
   Friction thermal sca.    tstar :  0.11614E+01 0.18600E+03
   Rough dim-less th. sca.  tplus :  0.72683E-02 0.20790E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27920E+00       9   0.60094E-05   0.18410E+01 0.22241E+02 
c  Velocity[X]                                      0.81139E+00 
c  Velocity[Y]                                      0.48206E+00 
c  Velocity[Z]                                      0.54756E+00 
c  Pressure     0.10788E-04      16   0.19254E-03   0.10588E-01 0.11628E+02 
c  k            0.12806E-01      11   0.15262E-04   0.25446E-01 0.41716E+02 
c  omega        0.27922E+07       1   0.57504E-07   0.33446E+07 0.33612E+00 
c  TempK        0.10045E+05       6   0.30151E-05   0.18359E+02 0.15059E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7055e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.254          19.213      -0.0022167       -0.012533
v  Velocity[Y]             -15.419           14.89         0.14661         0.20732
v  Velocity[Z]             -25.622          12.204         -1.6612         -0.5091
v  ǁVelocityǁ         0.00017646          25.798          7.7737          6.7714
v  Pressure                -518.72          204.11          26.686          29.722
v  k                   1.0016e-010          7.5852          0.1622         0.33025
v  omega                     57.49     2.7321e+008     1.2912e+006           76897
v  TempK                    298.45          363.17          334.08          340.08
v  TurbVisc            2.5103e-018      0.00091408     3.9693e-005      0.00014006
v  CourantNb            0.00014946          1.4913         0.79583          0.9763
v  FourierNb             0.0037456               1         0.39929         0.13315
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0039725     7.3028e-005       0.0001959

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.14           306.3
v  Yplus               0          2.9347         0.63504         0.49305


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62879          2.0797          1.1951          1.1094


 INSTANT    0.526000000E-02   TIME STEP NUMBER             526
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925325E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15181E-01 0.46823E+01
   Friction velocity        uk    :  0.15181E-01 0.46783E+01
   Dimensionless distance   yplus :  0.10293E-01 0.29346E+01
   Friction thermal sca.    tstar :  0.11634E+01 0.16763E+03
   Rough dim-less th. sca.  tplus :  0.72915E-02 0.20789E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27920E+00       9   0.60305E-05   0.18494E+01 0.22296E+02 
c  Velocity[X]                                      0.81399E+00 
c  Velocity[Y]                                      0.48328E+00 
c  Velocity[Z]                                      0.55216E+00 
c  Pressure     0.10479E-04      15   0.19363E-03   0.10286E-01 0.94330E+01 
c  k            0.12837E-01      11   0.15427E-04   0.25625E-01 0.41707E+02 
c  omega        0.27922E+07       1   0.59800E-07   0.62476E+07 0.41788E+00 
c  TempK        0.10046E+05       6   0.30070E-05   0.18251E+02 0.15010E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7052e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.254           19.21      -0.0022991       -0.012531
v  Velocity[Y]             -15.525           14.89          0.1469         0.20795
v  Velocity[Z]              -25.62          12.205         -1.6612        -0.50909
v  ǁVelocityǁ         0.00017752          25.796          7.7735           6.771
v  Pressure                -519.11          204.06          26.648          29.688
v  k                   1.0015e-010          7.5962         0.16251         0.33101
v  omega                     57.49     2.7321e+008     1.2912e+006           76897
v  TempK                    298.45          363.17           334.1          340.12
v  TurbVisc            2.5099e-018      0.00091174     3.9767e-005      0.00014034
v  CourantNb            0.00014941          1.4914         0.79582         0.97629
v  FourierNb             0.0037456               1         0.39936         0.13332
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.004205     7.3031e-005      0.00019593

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.14           306.3
v  Yplus               0          2.9346         0.63504         0.49304


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73965          2.0798          1.1952          1.1096


 INSTANT    0.527000000E-02   TIME STEP NUMBER             527
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925611E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15242E-01 0.46823E+01
   Friction velocity        uk    :  0.15242E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10334E-01 0.29344E+01
   Friction thermal sca.    tstar :  0.11653E+01 0.16696E+03
   Rough dim-less th. sca.  tplus :  0.73207E-02 0.20787E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27920E+00       9   0.60578E-05   0.18570E+01 0.22363E+02 
c  Velocity[X]                                      0.81726E+00 
c  Velocity[Y]                                      0.48689E+00 
c  Velocity[Z]                                      0.55282E+00 
c  Pressure     0.10259E-04      16   0.19517E-03   0.10069E-01 0.10085E+02 
c  k            0.12868E-01      11   0.15563E-04   0.25887E-01 0.41774E+02 
c  omega        0.27922E+07       1   0.65432E-07   0.17020E+08 0.64041E+00 
c  TempK        0.10047E+05       6   0.29988E-05   0.18142E+02 0.14962E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7047e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.254          19.207      -0.0023774       -0.012528
v  Velocity[Y]             -15.588           14.89         0.14718         0.20857
v  Velocity[Z]             -25.618          12.206         -1.6612        -0.50908
v  ǁVelocityǁ          0.0001785          25.793          7.7733          6.7705
v  Pressure                -519.51          204.01          26.603          29.647
v  k                   1.0013e-010          7.6067         0.16281         0.33177
v  omega                     57.49     2.7321e+008     1.2912e+006           76897
v  TempK                    298.45          363.17          334.12          340.15
v  TurbVisc            2.5095e-018      0.00090932     3.9841e-005      0.00014062
v  CourantNb            0.00014935          1.4915          0.7958         0.97629
v  FourierNb             0.0037457               1         0.39942          0.1335
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.003839     7.3035e-005      0.00019595

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.14           306.3
v  Yplus               0          2.9344         0.63504         0.49302


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75381            2.08          1.1952          1.1098


 INSTANT    0.528000000E-02   TIME STEP NUMBER             528
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925480E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15297E-01 0.46823E+01
   Friction velocity        uk    :  0.15297E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10371E-01 0.29342E+01
   Friction thermal sca.    tstar :  0.11673E+01 0.16636E+03
   Rough dim-less th. sca.  tplus :  0.73472E-02 0.20786E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27919E+00       9   0.60894E-05   0.18677E+01 0.22442E+02 
c  Velocity[X]                                      0.81948E+00 
c  Velocity[Y]                                      0.49181E+00 
c  Velocity[Z]                                      0.55642E+00 
c  Pressure     0.10175E-04      16   0.19150E-03   0.99868E-02 0.94687E+01 
c  k            0.12899E-01      11   0.15743E-04   0.26111E-01 0.41794E+02 
c  omega        0.27922E+07       1   0.65203E-07   0.14848E+08 0.60250E+00 
c  TempK        0.10048E+05       6   0.29906E-05   0.18037E+02 0.14914E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.705e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255          19.204      -0.0024552       -0.012524
v  Velocity[Y]             -15.527           14.89         0.14747          0.2092
v  Velocity[Z]             -25.615          12.207         -1.6612        -0.50907
v  ǁVelocityǁ         0.00017898          25.791          7.7731          6.7701
v  Pressure                 -519.9          203.97          26.565          29.613
v  k                   1.0012e-010          7.6166         0.16311         0.33254
v  omega                     57.49     2.7321e+008     1.2912e+006           76897
v  TempK                    298.45          363.17          334.14          340.19
v  TurbVisc            2.5092e-018      0.00090682     3.9915e-005      0.00014091
v  CourantNb             0.0001493          1.4914         0.79578         0.97628
v  FourierNb             0.0037459               1         0.39949         0.13367
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0036858     7.3039e-005      0.00019598

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.14           306.3
v  Yplus               0          2.9342         0.63504         0.49301


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64133            2.08          1.1953          1.1099


 INSTANT    0.529000000E-02   TIME STEP NUMBER             529
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925632E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15325E-01 0.46823E+01
   Friction velocity        uk    :  0.15325E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10390E-01 0.29340E+01
   Friction thermal sca.    tstar :  0.11693E+01 0.16606E+03
   Rough dim-less th. sca.  tplus :  0.73606E-02 0.20785E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27919E+00       9   0.61159E-05   0.18763E+01 0.22473E+02 
c  Velocity[X]                                      0.82487E+00 
c  Velocity[Y]                                      0.49309E+00 
c  Velocity[Z]                                      0.55835E+00 
c  Pressure     0.10325E-04      16   0.19632E-03   0.10134E-01 0.10218E+02 
c  k            0.12930E-01      11   0.15834E-04   0.26368E-01 0.41852E+02 
c  omega        0.27922E+07       1   0.61128E-07   0.79315E+07 0.46580E+00 
c  TempK        0.10049E+05       6   0.29825E-05   0.17932E+02 0.14866E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7054e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255          19.201      -0.0025291       -0.012519
v  Velocity[Y]             -15.482          14.891         0.14775         0.20982
v  Velocity[Z]             -25.613          12.208         -1.6611        -0.50906
v  ǁVelocityǁ         0.00018019          25.788          7.7729          6.7697
v  Pressure                -520.29          203.92          26.517           29.57
v  k                    1.001e-010           7.626         0.16342          0.3333
v  omega                     57.49     2.7321e+008     1.2912e+006           76897
v  TempK                    298.45          363.17          334.16          340.22
v  TurbVisc            2.5088e-018      0.00090427      3.999e-005      0.00014119
v  CourantNb            0.00014928          1.4913         0.79577         0.97627
v  FourierNb             0.0037463               1         0.39956         0.13385
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0037032     7.3043e-005      0.00019601

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.15           306.3
v  Yplus               0           2.934         0.63503         0.49299


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70411            2.08          1.1953          1.1101


 INSTANT    0.530000000E-02   TIME STEP NUMBER             530
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925557E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15392E-01 0.46823E+01
   Friction velocity        uk    :  0.15392E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10436E-01 0.29338E+01
   Friction thermal sca.    tstar :  0.11712E+01 0.16533E+03
   Rough dim-less th. sca.  tplus :  0.73930E-02 0.20783E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27919E+00       9   0.61428E-05   0.18836E+01 0.22465E+02 
c  Velocity[X]                                      0.83029E+00 
c  Velocity[Y]                                      0.49260E+00 
c  Velocity[Z]                                      0.56067E+00 
c  Pressure     0.10542E-04      16   0.19644E-03   0.10346E-01 0.94829E+01 
c  k            0.12961E-01      11   0.15925E-04   0.26667E-01 0.41940E+02 
c  omega        0.27922E+07       1   0.61316E-07   0.82133E+07 0.47477E+00 
c  TempK        0.10050E+05       6   0.29744E-05   0.17827E+02 0.14818E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7055e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255          19.198      -0.0026031       -0.012515
v  Velocity[Y]             -15.486          14.891         0.14804         0.21045
v  Velocity[Z]              -25.61           12.21         -1.6611        -0.50905
v  ǁVelocityǁ         0.00018143          25.786          7.7727          6.7692
v  Pressure                -520.67          203.87          26.476          29.533
v  k                   1.0009e-010          7.6347         0.16372         0.33406
v  omega                     57.49     2.7321e+008     1.2912e+006           76897
v  TempK                    298.45          363.17          334.18          340.25
v  TurbVisc            2.5085e-018      0.00090166     4.0064e-005      0.00014147
v  CourantNb            0.00014922          1.4913         0.79575         0.97626
v  FourierNb             0.0037468               1         0.39963         0.13402
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0037172     7.3046e-005      0.00019604

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.15          306.31
v  Yplus               0          2.9338         0.63502         0.49298


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61393            2.08          1.1954          1.1103


 INSTANT    0.531000000E-02   TIME STEP NUMBER             531
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925639E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15461E-01 0.46823E+01
   Friction velocity        uk    :  0.15461E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10483E-01 0.29337E+01
   Friction thermal sca.    tstar :  0.11732E+01 0.16460E+03
   Rough dim-less th. sca.  tplus :  0.74260E-02 0.20782E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27918E+00       9   0.61693E-05   0.18992E+01 0.22524E+02 
c  Velocity[X]                                      0.83792E+00 
c  Velocity[Y]                                      0.49402E+00 
c  Velocity[Z]                                      0.56723E+00 
c  Pressure     0.10932E-04      16   0.20000E-03   0.10730E-01 0.92368E+01 
c  k            0.12992E-01      11   0.16053E-04   0.26835E-01 0.41892E+02 
c  omega        0.27922E+07       1   0.60818E-07   0.66685E+07 0.43050E+00 
c  TempK        0.10051E+05       6   0.29663E-05   0.17723E+02 0.14771E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7053e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255          19.194      -0.0026763       -0.012509
v  Velocity[Y]             -15.583          14.892         0.14832         0.21107
v  Velocity[Z]             -25.608          12.211         -1.6611        -0.50904
v  ǁVelocityǁ          0.0001831          25.783          7.7725          6.7688
v  Pressure                -521.03          203.83          26.437          29.499
v  k                   1.0008e-010          7.6429         0.16403         0.33482
v  omega                     57.49     2.7321e+008     1.2912e+006           76898
v  TempK                    298.45          363.17           334.2          340.29
v  TurbVisc            2.5081e-018        0.000899     4.0139e-005      0.00014175
v  CourantNb            0.00014915          1.4914         0.79573         0.97626
v  FourierNb             0.0037474               1          0.3997          0.1342
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0037261     7.3049e-005      0.00019607

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.15          306.31
v  Yplus               0          2.9337         0.63502         0.49297


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59734          2.0801          1.1954          1.1105


 INSTANT    0.532000000E-02   TIME STEP NUMBER             532
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925640E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15553E-01 0.46823E+01
   Friction velocity        uk    :  0.15553E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10545E-01 0.29335E+01
   Friction thermal sca.    tstar :  0.11752E+01 0.16362E+03
   Rough dim-less th. sca.  tplus :  0.74703E-02 0.20781E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27918E+00       9   0.61939E-05   0.19153E+01 0.22605E+02 
c  Velocity[X]                                      0.84572E+00 
c  Velocity[Y]                                      0.49849E+00 
c  Velocity[Z]                                      0.57107E+00 
c  Pressure     0.10776E-04      16   0.19789E-03   0.10575E-01 0.85211E+01 
c  k            0.13023E-01      11   0.16184E-04   0.27084E-01 0.41921E+02 
c  omega        0.27922E+07       1   0.64541E-07   0.14695E+08 0.60254E+00 
c  TempK        0.10052E+05       6   0.29582E-05   0.17620E+02 0.14724E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.705e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.191      -0.0027461       -0.012503
v  Velocity[Y]             -15.638          14.892          0.1486         0.21169
v  Velocity[Z]             -25.606          12.212          -1.661        -0.50903
v  ǁVelocityǁ         0.00018451          25.781          7.7723          6.7683
v  Pressure                -521.38          203.79          26.406          29.472
v  k                   1.0006e-010          7.6504         0.16433         0.33558
v  omega                     57.49     2.7321e+008     1.2912e+006           76898
v  TempK                    298.45          363.17          334.22          340.32
v  TurbVisc            2.5078e-018      0.00089631     4.0214e-005      0.00014203
v  CourantNb            0.00014905          1.4914         0.79571         0.97625
v  FourierNb             0.0037478               1         0.39977         0.13438
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0037314     7.3052e-005       0.0001961

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.15          306.31
v  Yplus               0          2.9335         0.63502         0.49295


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47765          2.0803          1.1955          1.1106


 INSTANT    0.533000000E-02   TIME STEP NUMBER             533
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925656E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15630E-01 0.46823E+01
   Friction velocity        uk    :  0.15630E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10598E-01 0.29333E+01
   Friction thermal sca.    tstar :  0.11772E+01 0.16282E+03
   Rough dim-less th. sca.  tplus :  0.75074E-02 0.20780E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27917E+00       9   0.62195E-05   0.19263E+01 0.22663E+02 
c  Velocity[X]                                      0.85365E+00 
c  Velocity[Y]                                      0.50303E+00 
c  Velocity[Z]                                      0.56966E+00 
c  Pressure     0.10773E-04      15   0.19874E-03   0.10573E-01 0.88072E+01 
c  k            0.13053E-01      11   0.16268E-04   0.27290E-01 0.41904E+02 
c  omega        0.27922E+07       1   0.61962E-07   0.93170E+07 0.49741E+00 
c  TempK        0.10053E+05       6   0.29502E-05   0.17518E+02 0.14677E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7053e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.188      -0.0028159       -0.012497
v  Velocity[Y]             -15.569          14.892         0.14888         0.21231
v  Velocity[Z]             -25.604          12.212          -1.661        -0.50901
v  ǁVelocityǁ         0.00018639          25.779          7.7721          6.7679
v  Pressure                -521.72          203.75          26.371          29.442
v  k                   1.0005e-010          7.6572         0.16463         0.33634
v  omega                     57.49     2.7322e+008     1.2912e+006           76898
v  TempK                    298.45          363.17          334.24          340.36
v  TurbVisc            2.5074e-018      0.00089358     4.0289e-005      0.00014231
v  CourantNb            0.00014898          1.4913          0.7957         0.97624
v  FourierNb              0.003748               1         0.39984         0.13455
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0037347     7.3055e-005      0.00019613

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.15          306.31
v  Yplus               0          2.9333         0.63501         0.49294


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63235          2.0803          1.1955          1.1108


 INSTANT    0.534000000E-02   TIME STEP NUMBER             534
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925672E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15732E-01 0.46823E+01
   Friction velocity        uk    :  0.15732E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10667E-01 0.29331E+01
   Friction thermal sca.    tstar :  0.11792E+01 0.16176E+03
   Rough dim-less th. sca.  tplus :  0.75563E-02 0.20779E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27916E+00       9   0.62561E-05   0.19396E+01 0.22674E+02 
c  Velocity[X]                                      0.86244E+00 
c  Velocity[Y]                                      0.50163E+00 
c  Velocity[Z]                                      0.57553E+00 
c  Pressure     0.11174E-04      15   0.20030E-03   0.10965E-01 0.86194E+01 
c  k            0.13084E-01      11   0.16403E-04   0.27534E-01 0.41924E+02 
c  omega        0.27922E+07       1   0.60344E-07   0.58680E+07 0.41086E+00 
c  TempK        0.10054E+05       6   0.29421E-05   0.17420E+02 0.14632E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7058e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.185      -0.0028848       -0.012489
v  Velocity[Y]             -15.517          14.893         0.14916         0.21293
v  Velocity[Z]             -25.601          12.213         -1.6609          -0.509
v  ǁVelocityǁ         0.00018759          25.777          7.7719          6.7674
v  Pressure                -522.06          203.71          26.338          29.414
v  k                   1.0003e-010          7.6635         0.16494         0.33711
v  omega                     57.49     2.7322e+008     1.2912e+006           76898
v  TempK                    298.45          363.17          334.26          340.39
v  TurbVisc            2.5071e-018      0.00089081     4.0363e-005      0.00014259
v  CourantNb            0.00014887          1.4913         0.79568         0.97623
v  FourierNb             0.0037481               1         0.39991         0.13473
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0037323     7.3059e-005      0.00019616

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.16          306.31
v  Yplus               0          2.9331         0.63501         0.49293


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52084          2.0803          1.1956           1.111


 INSTANT    0.535000000E-02   TIME STEP NUMBER             535
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925681E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15797E-01 0.46823E+01
   Friction velocity        uk    :  0.15797E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10711E-01 0.29330E+01
   Friction thermal sca.    tstar :  0.11811E+01 0.16110E+03
   Rough dim-less th. sca.  tplus :  0.75876E-02 0.20777E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27916E+00       9   0.62972E-05   0.19581E+01 0.22778E+02 
c  Velocity[X]                                      0.87015E+00 
c  Velocity[Y]                                      0.50716E+00 
c  Velocity[Z]                                      0.58075E+00 
c  Pressure     0.10988E-04      15   0.20197E-03   0.10782E-01 0.82642E+01 
c  k            0.13115E-01      11   0.16638E-04   0.27780E-01 0.41962E+02 
c  omega        0.27922E+07       1   0.62476E-07   0.85626E+07 0.47796E+00 
c  TempK        0.10055E+05       6   0.29341E-05   0.17322E+02 0.14587E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7059e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.182      -0.0029505       -0.012482
v  Velocity[Y]             -15.514          14.894         0.14944         0.21355
v  Velocity[Z]             -25.599          12.214         -1.6609        -0.50899
v  ǁVelocityǁ         0.00018928          25.775          7.7717          6.7669
v  Pressure                -522.38          203.68          26.312          29.391
v  k                   1.0002e-010          7.9296         0.16524         0.33787
v  omega                     57.49     2.7322e+008     1.2912e+006           76898
v  TempK                    298.46          363.17          334.28          340.43
v  TurbVisc            2.5067e-018      0.00088801     4.0438e-005      0.00014287
v  CourantNb            0.00014882          1.4912         0.79566         0.97623
v  FourierNb             0.0037482               1         0.39998         0.13491
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0037253     7.3063e-005      0.00019619

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.16          306.31
v  Yplus               0           2.933         0.63501         0.49291


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75457          2.0803          1.1956          1.1111


 INSTANT    0.536000000E-02   TIME STEP NUMBER             536
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925576E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15887E-01 0.46824E+01
   Friction velocity        uk    :  0.15887E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10772E-01 0.29328E+01
   Friction thermal sca.    tstar :  0.11831E+01 0.16019E+03
   Rough dim-less th. sca.  tplus :  0.76308E-02 0.20776E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27915E+00       9   0.63341E-05   0.19651E+01 0.22855E+02 
c  Velocity[X]                                      0.87607E+00 
c  Velocity[Y]                                      0.51025E+00 
c  Velocity[Z]                                      0.57879E+00 
c  Pressure     0.10855E-04      15   0.20533E-03   0.10650E-01 0.84003E+01 
c  k            0.13145E-01      11   0.16687E-04   0.27832E-01 0.41808E+02 
c  omega        0.27922E+07       1   0.63408E-07   0.10046E+08 0.50979E+00 
c  TempK        0.10056E+05       6   0.29261E-05   0.17227E+02 0.14543E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7057e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.179      -0.0030172       -0.012475
v  Velocity[Y]             -15.606          14.894         0.14971         0.21417
v  Velocity[Z]             -25.597          12.215         -1.6609        -0.50898
v  ǁVelocityǁ         0.00019058          25.772          7.7714          6.7664
v  Pressure                -522.69          203.64          26.282          29.367
v  k                   1.0001e-010          7.7561         0.16555         0.33863
v  omega                     57.49     2.7322e+008     1.2912e+006           76898
v  TempK                    298.46          363.17           334.3          340.46
v  TurbVisc            2.5064e-018      0.00088519     4.0514e-005      0.00014316
v  CourantNb            0.00014874          1.4913         0.79565         0.97622
v  FourierNb             0.0037484               1         0.40005         0.13509
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0037137     7.3068e-005      0.00019622

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.16          306.31
v  Yplus               0          2.9328           0.635          0.4929


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68033          2.0804          1.1957          1.1113


 INSTANT    0.537000000E-02   TIME STEP NUMBER             537
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925541E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15955E-01 0.46824E+01
   Friction velocity        uk    :  0.15955E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10818E-01 0.29326E+01
   Friction thermal sca.    tstar :  0.11852E+01 0.15950E+03
   Rough dim-less th. sca.  tplus :  0.76635E-02 0.20775E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27914E+00       9   0.63668E-05   0.19808E+01 0.22921E+02 
c  Velocity[X]                                      0.88246E+00 
c  Velocity[Y]                                      0.51447E+00 
c  Velocity[Z]                                      0.58383E+00 
c  Pressure     0.10961E-04      15   0.20797E-03   0.10754E-01 0.82237E+01 
c  k            0.13176E-01      11   0.16747E-04   0.28018E-01 0.41791E+02 
c  omega        0.27922E+07       1   0.67008E-07   0.18678E+08 0.67095E+00 
c  TempK        0.10056E+05       6   0.29181E-05   0.17130E+02 0.14498E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7054e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.177      -0.0030833       -0.012469
v  Velocity[Y]             -15.655          14.894         0.14998         0.21479
v  Velocity[Z]             -25.594          12.216         -1.6608        -0.50896
v  ǁVelocityǁ         0.00019321           25.77          7.7712          6.7659
v  Pressure                -522.98          203.61          26.255          29.344
v  k                   9.9993e-011          7.6787         0.16585         0.33939
v  omega                     57.49     2.7322e+008     1.2912e+006           76899
v  TempK                    298.46          363.17          334.32          340.49
v  TurbVisc             2.506e-018      0.00088234     4.0589e-005      0.00014344
v  CourantNb            0.00014869          1.4913         0.79563         0.97621
v  FourierNb             0.0037487               1         0.40012         0.13528
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0036913     7.3072e-005      0.00019625

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.16          306.31
v  Yplus               0          2.9326           0.635         0.49288


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51254          2.0805          1.1958          1.1115


 INSTANT    0.538000000E-02   TIME STEP NUMBER             538
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925622E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16094E-01 0.46824E+01
   Friction velocity        uk    :  0.16094E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10912E-01 0.29324E+01
   Friction thermal sca.    tstar :  0.11872E+01 0.15813E+03
   Rough dim-less th. sca.  tplus :  0.77299E-02 0.20773E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27913E+00       9   0.64260E-05   0.19907E+01 0.22957E+02 
c  Velocity[X]                                      0.88790E+00 
c  Velocity[Y]                                      0.51802E+00 
c  Velocity[Z]                                      0.58482E+00 
c  Pressure     0.10843E-04      14   0.20673E-03   0.10638E-01 0.84128E+01 
c  k            0.13206E-01      11   0.16893E-04   0.28222E-01 0.41794E+02 
c  omega        0.27922E+07       1   0.62446E-07   0.94086E+07 0.49614E+00 
c  TempK        0.10057E+05       6   0.29102E-05   0.17034E+02 0.14454E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7057e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.174      -0.0031511       -0.012465
v  Velocity[Y]              -15.58          14.895         0.15026          0.2154
v  Velocity[Z]             -25.592          12.216         -1.6608        -0.50895
v  ǁVelocityǁ         0.00019481          25.768           7.771          6.7654
v  Pressure                -523.27          203.58          26.225          29.319
v  k                    9.998e-011          7.6827         0.16616         0.34015
v  omega                     57.49     2.7322e+008     1.2912e+006           76899
v  TempK                    298.46          363.17          334.34          340.53
v  TurbVisc            2.5057e-018      0.00087947     4.0664e-005      0.00014372
v  CourantNb            0.00014854          1.4913         0.79561          0.9762
v  FourierNb             0.0037493               1          0.4002         0.13546
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0036563     7.3076e-005      0.00019628

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.16          306.32
v  Yplus               0          2.9324         0.63499         0.49287


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50931          2.0805          1.1958          1.1117


 INSTANT    0.539000000E-02   TIME STEP NUMBER             539
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925688E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16177E-01 0.46824E+01
   Friction velocity        uk    :  0.16177E-01 0.46784E+01
   Dimensionless distance   yplus :  0.10968E-01 0.29323E+01
   Friction thermal sca.    tstar :  0.11892E+01 0.15731E+03
   Rough dim-less th. sca.  tplus :  0.77701E-02 0.20772E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27912E+00       9   0.64403E-05   0.19974E+01 0.22942E+02 
c  Velocity[X]                                      0.89363E+00 
c  Velocity[Y]                                      0.51644E+00 
c  Velocity[Z]                                      0.58734E+00 
c  Pressure     0.11002E-04      14   0.21240E-03   0.10792E-01 0.81793E+01 
c  k            0.13237E-01      11   0.17022E-04   0.28439E-01 0.41807E+02 
c  omega        0.27922E+07       1   0.59034E-07   0.33981E+07 0.33582E+00 
c  TempK        0.10058E+05       6   0.29022E-05   0.16940E+02 0.14410E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7061e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.171      -0.0032178        -0.01246
v  Velocity[Y]             -15.522          14.895         0.15052         0.21601
v  Velocity[Z]              -25.59          12.217         -1.6607        -0.50894
v  ǁVelocityǁ         0.00019734          25.766          7.7707          6.7649
v  Pressure                -523.55          203.54          26.198          29.297
v  k                   9.9967e-011          7.7636         0.16646         0.34091
v  omega                     57.49     2.7322e+008     1.2912e+006           76899
v  TempK                    298.46          363.17          334.36          340.56
v  TurbVisc            2.5054e-018       0.0008766     4.0739e-005        0.000144
v  CourantNb            0.00014847          1.4912         0.79559         0.97619
v  FourierNb             0.0037498               1         0.40027         0.13564
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0036139      7.308e-005      0.00019631

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.16          306.32
v  Yplus               0          2.9323         0.63499         0.49285


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.539          2.0805          1.1959          1.1118


 INSTANT    0.540000000E-02   TIME STEP NUMBER             540
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925650E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16307E-01 0.46824E+01
   Friction velocity        uk    :  0.16307E-01 0.46784E+01
   Dimensionless distance   yplus :  0.11057E-01 0.29321E+01
   Friction thermal sca.    tstar :  0.11912E+01 0.15606E+03
   Rough dim-less th. sca.  tplus :  0.78325E-02 0.20771E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27911E+00       9   0.64677E-05   0.20087E+01 0.22983E+02 
c  Velocity[X]                                      0.89947E+00 
c  Velocity[Y]                                      0.51897E+00 
c  Velocity[Z]                                      0.59023E+00 
c  Pressure     0.11118E-04      14   0.21685E-03   0.10906E-01 0.79238E+01 
c  k            0.13267E-01      11   0.17208E-04   0.28589E-01 0.41732E+02 
c  omega        0.27922E+07       1   0.59005E-07   0.32834E+07 0.33222E+00 
c  TempK        0.10059E+05       6   0.28942E-05   0.16848E+02 0.14366E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7062e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.169      -0.0032819       -0.012457
v  Velocity[Y]             -15.515          14.896         0.15079         0.21663
v  Velocity[Z]             -25.588          12.218         -1.6607        -0.50893
v  ǁVelocityǁ         0.00019886          25.764          7.7705          6.7643
v  Pressure                -523.82          203.51          26.173          29.277
v  k                   9.9953e-011          7.7262         0.16677         0.34167
v  omega                     57.49     2.7322e+008     1.2912e+006           76899
v  TempK                    298.46          363.17          334.38           340.6
v  TurbVisc             2.505e-018      0.00087323     4.0815e-005      0.00014428
v  CourantNb            0.00014833          1.4912         0.79557         0.97619
v  FourierNb             0.0037502               1         0.40034         0.13582
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0035642     7.3083e-005      0.00019634

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.17          306.32
v  Yplus               0          2.9321         0.63498         0.49284


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65728          2.0806          1.1959           1.112


 INSTANT    0.541000000E-02   TIME STEP NUMBER             541
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925618E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16384E-01 0.46824E+01
   Friction velocity        uk    :  0.16384E-01 0.46784E+01
   Dimensionless distance   yplus :  0.11109E-01 0.29319E+01
   Friction thermal sca.    tstar :  0.11933E+01 0.15533E+03
   Rough dim-less th. sca.  tplus :  0.78694E-02 0.20770E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27910E+00       9   0.65113E-05   0.20182E+01 0.23030E+02 
c  Velocity[X]                                      0.90505E+00 
c  Velocity[Y]                                      0.52203E+00 
c  Velocity[Z]                                      0.59108E+00 
c  Pressure     0.11090E-04      14   0.21619E-03   0.10877E-01 0.75505E+01 
c  k            0.13298E-01      11   0.17409E-04   0.28751E-01 0.41667E+02 
c  omega        0.27922E+07       1   0.62131E-07   0.78092E+07 0.45454E+00 
c  TempK        0.10060E+05       6   0.28862E-05   0.16756E+02 0.14323E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7059e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.167      -0.0033443       -0.012453
v  Velocity[Y]             -15.574          14.897         0.15106         0.21724
v  Velocity[Z]             -25.586          12.218         -1.6606        -0.50892
v  ǁVelocityǁ         0.00020164          25.762          7.7702          6.7638
v  Pressure                -524.06          203.49          26.153          29.262
v  k                    9.994e-011          7.6918         0.16707         0.34243
v  omega                     57.49     2.7322e+008     1.2912e+006           76899
v  TempK                    298.46          363.17           334.4          340.63
v  TurbVisc            2.5047e-018      0.00086969      4.089e-005      0.00014456
v  CourantNb            0.00014827          1.4912         0.79555         0.97618
v  FourierNb             0.0037505               1         0.40041           0.136
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0035223     7.3087e-005      0.00019637

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.17          306.32
v  Yplus               0          2.9319         0.63498         0.49282


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70137          2.0807           1.196          1.1122


 INSTANT    0.542000000E-02   TIME STEP NUMBER             542
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925556E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16525E-01 0.46824E+01
   Friction velocity        uk    :  0.16525E-01 0.46784E+01
   Dimensionless distance   yplus :  0.11204E-01 0.29318E+01
   Friction thermal sca.    tstar :  0.11953E+01 0.15401E+03
   Rough dim-less th. sca.  tplus :  0.79370E-02 0.20769E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27909E+00       9   0.65711E-05   0.20345E+01 0.23140E+02 
c  Velocity[X]                                      0.91021E+00 
c  Velocity[Y]                                      0.52778E+00 
c  Velocity[Z]                                      0.59649E+00 
c  Pressure     0.11157E-04      14   0.21900E-03   0.10943E-01 0.74438E+01 
c  k            0.13328E-01      11   0.17596E-04   0.28945E-01 0.41630E+02 
c  omega        0.27922E+07       1   0.67177E-07   0.15190E+08 0.60327E+00 
c  TempK        0.10060E+05       6   0.28783E-05   0.16665E+02 0.14281E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7053e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258          19.164      -0.0034029        -0.01245
v  Velocity[Y]             -15.642          14.897         0.15133         0.21785
v  Velocity[Z]             -25.584          12.219         -1.6606        -0.50891
v  ǁVelocityǁ          0.0002039           25.76          7.7699          6.7632
v  Pressure                -524.29          203.47          26.142          29.256
v  k                   9.9927e-011           7.694         0.16738         0.34319
v  omega                     57.49     2.7322e+008     1.2912e+006           76899
v  TempK                    298.46          363.17          334.42          340.66
v  TurbVisc            2.5044e-018      0.00086608     4.0966e-005      0.00014485
v  CourantNb            0.00014812          1.4914         0.79553         0.97617
v  FourierNb             0.0037505               1         0.40049         0.13618
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.003489     7.3091e-005       0.0001964

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.17          306.32
v  Yplus               0          2.9318         0.63498         0.49281


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77337          2.0809           1.196          1.1123


 INSTANT    0.543000000E-02   TIME STEP NUMBER             543
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925444E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16637E-01 0.46824E+01
   Friction velocity        uk    :  0.16637E-01 0.46784E+01
   Dimensionless distance   yplus :  0.11280E-01 0.29316E+01
   Friction thermal sca.    tstar :  0.11974E+01 0.15296E+03
   Rough dim-less th. sca.  tplus :  0.79911E-02 0.20768E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27908E+00       9   0.66330E-05   0.20541E+01 0.23264E+02 
c  Velocity[X]                                      0.91777E+00 
c  Velocity[Y]                                      0.53743E+00 
c  Velocity[Z]                                      0.59895E+00 
c  Pressure     0.11228E-04      14   0.21653E-03   0.11012E-01 0.74671E+01 
c  k            0.13358E-01      11   0.17779E-04   0.29149E-01 0.41582E+02 
c  omega        0.27922E+07       1   0.65604E-07   0.13945E+08 0.59184E+00 
c  TempK        0.10061E+05       6   0.28704E-05   0.16572E+02 0.14237E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7055e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258          19.162        -0.00346       -0.012446
v  Velocity[Y]             -15.611          14.897          0.1516         0.21846
v  Velocity[Z]             -25.582           12.22         -1.6605         -0.5089
v  ǁVelocityǁ         0.00020604          25.757          7.7696          6.7627
v  Pressure                -524.51          203.45          26.124          29.243
v  k                   9.9914e-011          7.6959         0.16768         0.34394
v  omega                     57.49     2.7322e+008     1.2912e+006           76899
v  TempK                    298.46          363.17          334.43           340.7
v  TurbVisc             2.504e-018      0.00086797     4.1041e-005      0.00014513
v  CourantNb            0.00014802          1.4913         0.79551         0.97616
v  FourierNb             0.0037506               1         0.40056         0.13637
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0034778     7.3095e-005      0.00019643

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.17          306.32
v  Yplus               0          2.9316         0.63497         0.49279


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6334          2.0809          1.1961          1.1125


 INSTANT    0.544000000E-02   TIME STEP NUMBER             544
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925525E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16743E-01 0.46823E+01
   Friction velocity        uk    :  0.16743E-01 0.46784E+01
   Dimensionless distance   yplus :  0.11352E-01 0.29314E+01
   Friction thermal sca.    tstar :  0.11995E+01 0.15200E+03
   Rough dim-less th. sca.  tplus :  0.80418E-02 0.20766E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27907E+00       9   0.66689E-05   0.20600E+01 0.23218E+02 
c  Velocity[X]                                      0.92398E+00 
c  Velocity[Y]                                      0.53463E+00 
c  Velocity[Z]                                      0.60139E+00 
c  Pressure     0.11460E-04      14   0.21115E-03   0.11239E-01 0.76848E+01 
c  k            0.13388E-01      11   0.17993E-04   0.29384E-01 0.41571E+02 
c  omega        0.27922E+07       1   0.63902E-07   0.11069E+08 0.53332E+00 
c  TempK        0.10062E+05       6   0.28625E-05   0.16479E+02 0.14193E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7059e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258           19.16      -0.0035158       -0.012441
v  Velocity[Y]             -15.513          14.898         0.15187         0.21907
v  Velocity[Z]              -25.58           12.22         -1.6605        -0.50889
v  ǁVelocityǁ         0.00020833          25.755          7.7693          6.7621
v  Pressure                -524.74          203.42          26.103          29.226
v  k                   9.9901e-011          7.7944         0.16798          0.3447
v  omega                    57.489     2.7322e+008     1.2912e+006           76900
v  TempK                    298.46          363.17          334.45          340.73
v  TurbVisc            2.5037e-018      0.00087184     4.1116e-005      0.00014541
v  CourantNb            0.00014792          1.4912         0.79549         0.97615
v  FourierNb             0.0037508               1         0.40063         0.13655
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.003736     7.3099e-005      0.00019647

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.17          306.32
v  Yplus               0          2.9314         0.63496         0.49277


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68501          2.0809          1.1961          1.1127


 INSTANT    0.545000000E-02   TIME STEP NUMBER             545
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925667E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16856E-01 0.46823E+01
   Friction velocity        uk    :  0.16856E-01 0.46784E+01
   Dimensionless distance   yplus :  0.11428E-01 0.29313E+01
   Friction thermal sca.    tstar :  0.12016E+01 0.15098E+03
   Rough dim-less th. sca.  tplus :  0.80960E-02 0.20765E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27905E+00       9   0.66604E-05   0.20697E+01 0.23236E+02 
c  Velocity[X]                                      0.93121E+00 
c  Velocity[Y]                                      0.53545E+00 
c  Velocity[Z]                                      0.60304E+00 
c  Pressure     0.11355E-04      14   0.20973E-03   0.11136E-01 0.76912E+01 
c  k            0.13418E-01      11   0.18161E-04   0.29698E-01 0.41636E+02 
c  omega        0.27922E+07       1   0.59543E-07   0.37632E+07 0.34255E+00 
c  TempK        0.10063E+05       6   0.28547E-05   0.16390E+02 0.14151E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.706e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258          19.158      -0.0035694       -0.012436
v  Velocity[Y]             -15.481          14.898         0.15214         0.21968
v  Velocity[Z]             -25.578          12.221         -1.6604        -0.50887
v  ǁVelocityǁ          0.0002113          25.753          7.7691          6.7615
v  Pressure                -524.94          203.39           26.08          29.209
v  k                   9.9888e-011          8.3471         0.16829         0.34546
v  omega                    57.489     2.7322e+008     1.2912e+006           76900
v  TempK                    298.46          363.17          334.47          340.76
v  TurbVisc            2.5034e-018      0.00087561     4.1192e-005      0.00014569
v  CourantNb            0.00014781          1.4912         0.79547         0.97614
v  FourierNb             0.0037512               1          0.4007         0.13673
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0039904     7.3104e-005       0.0001965

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.18          306.32
v  Yplus               0          2.9313         0.63495         0.49275


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7068           2.081          1.1962          1.1129


 INSTANT    0.546000000E-02   TIME STEP NUMBER             546
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925459E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16999E-01 0.46823E+01
   Friction velocity        uk    :  0.16999E-01 0.46784E+01
   Dimensionless distance   yplus :  0.11525E-01 0.29311E+01
   Friction thermal sca.    tstar :  0.12037E+01 0.14971E+03
   Rough dim-less th. sca.  tplus :  0.81646E-02 0.20764E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27904E+00       9   0.66916E-05   0.20860E+01 0.23292E+02 
c  Velocity[X]                                      0.94041E+00 
c  Velocity[Y]                                      0.53808E+00 
c  Velocity[Z]                                      0.60749E+00 
c  Pressure     0.11626E-04      14   0.21244E-03   0.11401E-01 0.71509E+01 
c  k            0.13448E-01      11   0.18292E-04   0.29807E-01 0.41503E+02 
c  omega        0.27922E+07       1   0.59203E-07   0.32892E+07 0.32792E+00 
c  TempK        0.10063E+05       6   0.28469E-05   0.16302E+02 0.14109E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7057e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258          19.156      -0.0036194       -0.012428
v  Velocity[Y]             -15.505          14.899         0.15241         0.22029
v  Velocity[Z]             -25.576          12.221         -1.6603        -0.50886
v  ǁVelocityǁ         0.00021364          25.752          7.7688           6.761
v  Pressure                -525.13          203.37          26.066            29.2
v  k                   9.9876e-011          8.2966         0.16859         0.34621
v  omega                    57.489     2.7322e+008     1.2912e+006           76900
v  TempK                    298.46          363.17          334.49          340.79
v  TurbVisc            2.5031e-018      0.00087925     4.1267e-005      0.00014597
v  CourantNb            0.00014766          1.4913         0.79545         0.97612
v  FourierNb             0.0037517               1         0.40078         0.13691
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040532     7.3109e-005      0.00019653

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.18          306.33
v  Yplus               0          2.9311         0.63495         0.49274


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66116          2.0811          1.1962           1.113


 INSTANT    0.547000000E-02   TIME STEP NUMBER             547
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925354E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17112E-01 0.46823E+01
   Friction velocity        uk    :  0.17112E-01 0.46784E+01
   Dimensionless distance   yplus :  0.11602E-01 0.29310E+01
   Friction thermal sca.    tstar :  0.12058E+01 0.14872E+03
   Rough dim-less th. sca.  tplus :  0.82189E-02 0.20763E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27903E+00       9   0.67348E-05   0.21025E+01 0.23364E+02 
c  Velocity[X]                                      0.94733E+00 
c  Velocity[Y]                                      0.54107E+00 
c  Velocity[Z]                                      0.61413E+00 
c  Pressure     0.11686E-04      15   0.21479E-03   0.11460E-01 0.70947E+01 
c  k            0.13478E-01      11   0.18453E-04   0.29988E-01 0.41471E+02 
c  omega        0.27922E+07       1   0.61794E-07   0.69930E+07 0.43116E+00 
c  TempK        0.10064E+05       6   0.28391E-05   0.16214E+02 0.14067E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7049e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258          19.154      -0.0036656       -0.012419
v  Velocity[Y]             -15.598          14.899         0.15268         0.22089
v  Velocity[Z]             -25.575          12.221         -1.6602        -0.50885
v  ǁVelocityǁ         0.00021648           25.75          7.7685          6.7604
v  Pressure                -525.31          203.36          26.055          29.195
v  k                   9.9863e-011          8.1873         0.16889         0.34697
v  omega                    57.489     2.7322e+008     1.2912e+006           76900
v  TempK                    298.46          363.17          334.51          340.83
v  TurbVisc            2.5027e-018      0.00088272     4.1343e-005      0.00014625
v  CourantNb            0.00014755          1.4914         0.79543         0.97611
v  FourierNb             0.0037522               1         0.40085          0.1371
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.003531     7.3114e-005      0.00019656

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.18          306.33
v  Yplus               0           2.931         0.63494         0.49272


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65061          2.0813          1.1963          1.1132


 INSTANT    0.548000000E-02   TIME STEP NUMBER             548
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925318E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17246E-01 0.46823E+01
   Friction velocity        uk    :  0.17246E-01 0.46784E+01
   Dimensionless distance   yplus :  0.11693E-01 0.29309E+01
   Friction thermal sca.    tstar :  0.12080E+01 0.14757E+03
   Rough dim-less th. sca.  tplus :  0.82834E-02 0.20762E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27901E+00       9   0.67740E-05   0.21195E+01 0.23458E+02 
c  Velocity[X]                                      0.95415E+00 
c  Velocity[Y]                                      0.54608E+00 
c  Velocity[Z]                                      0.61926E+00 
c  Pressure     0.12258E-04      15   0.21671E-03   0.12019E-01 0.70824E+01 
c  k            0.13508E-01      11   0.18661E-04   0.30233E-01 0.41490E+02 
c  omega        0.27922E+07       1   0.64499E-07   0.11779E+08 0.53693E+00 
c  TempK        0.10065E+05       6   0.28313E-05   0.16128E+02 0.14026E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7041e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258          19.153      -0.0037054       -0.012407
v  Velocity[Y]             -15.658          14.899         0.15295         0.22149
v  Velocity[Z]             -25.573          12.222         -1.6602        -0.50884
v  ǁVelocityǁ         0.00021886          25.748          7.7682          6.7598
v  Pressure                -525.47          203.34          26.044          29.189
v  k                    9.985e-011          7.9906          0.1692         0.34772
v  omega                    57.489     2.7322e+008     1.2912e+006           76900
v  TempK                    298.46          363.17          334.53          340.86
v  TurbVisc            2.5024e-018      0.00088601     4.1419e-005      0.00014653
v  CourantNb            0.00014742          1.4916         0.79541          0.9761
v  FourierNb             0.0037525               1         0.40092         0.13728
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0033504     7.3118e-005      0.00019659

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.18          306.33
v  Yplus               0          2.9309         0.63494          0.4927


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63552          2.0816          1.1963          1.1134


 INSTANT    0.549000000E-02   TIME STEP NUMBER             549
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925278E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17358E-01 0.46823E+01
   Friction velocity        uk    :  0.17358E-01 0.46784E+01
   Dimensionless distance   yplus :  0.11769E-01 0.29307E+01
   Friction thermal sca.    tstar :  0.12101E+01 0.14662E+03
   Rough dim-less th. sca.  tplus :  0.83371E-02 0.20761E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27900E+00       9   0.68101E-05   0.21351E+01 0.23574E+02 
c  Velocity[X]                                      0.96146E+00 
c  Velocity[Y]                                      0.55297E+00 
c  Velocity[Z]                                      0.62071E+00 
c  Pressure     0.11973E-04      15   0.21959E-03   0.11739E-01 0.75154E+01 
c  k            0.13538E-01      11   0.18938E-04   0.30444E-01 0.41465E+02 
c  omega        0.27922E+07       1   0.65975E-07   0.13293E+08 0.56723E+00 
c  TempK        0.10065E+05       6   0.28236E-05   0.16043E+02 0.13985E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.704e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258          19.151      -0.0037412       -0.012394
v  Velocity[Y]             -15.584            14.9         0.15323         0.22209
v  Velocity[Z]             -25.571          12.222         -1.6601        -0.50883
v  ǁVelocityǁ         0.00022157          25.746          7.7679          6.7592
v  Pressure                -525.62          203.33          26.038          29.187
v  k                   9.9838e-011          7.8512          0.1695         0.34848
v  omega                    57.489     2.7322e+008     1.2912e+006           76900
v  TempK                    298.46          363.17          334.55          340.89
v  TurbVisc            2.5021e-018      0.00088914     4.1494e-005      0.00014681
v  CourantNb            0.00014731          1.4916         0.79539         0.97609
v  FourierNb             0.0037528               1           0.401         0.13746
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0033261     7.3123e-005      0.00019662

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.18          306.33
v  Yplus               0          2.9307         0.63493         0.49268


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48774          2.0816          1.1964          1.1135


 INSTANT    0.550000000E-02   TIME STEP NUMBER             550
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925080E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17484E-01 0.46823E+01
   Friction velocity        uk    :  0.17484E-01 0.46784E+01
   Dimensionless distance   yplus :  0.11854E-01 0.29305E+01
   Friction thermal sca.    tstar :  0.12111E+01 0.14556E+03
   Rough dim-less th. sca.  tplus :  0.83977E-02 0.20760E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27898E+00       9   0.68631E-05   0.21500E+01 0.23612E+02 
c  Velocity[X]                                      0.97005E+00 
c  Velocity[Y]                                      0.55506E+00 
c  Velocity[Z]                                      0.62489E+00 
c  Pressure     0.13871E-04      14   0.22126E-03   0.13598E-01 0.71769E+01 
c  k            0.13568E-01      11   0.19136E-04   0.30707E-01 0.41499E+02 
c  omega        0.27922E+07       1   0.63330E-07   0.87705E+07 0.47258E+00 
c  TempK        0.10066E+05       6   0.28159E-05   0.15957E+02 0.13944E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.704e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258          19.149      -0.0037752       -0.012378
v  Velocity[Y]             -15.519            14.9         0.15351         0.22269
v  Velocity[Z]             -25.569          12.223           -1.66        -0.50881
v  ǁVelocityǁ         0.00022386          25.744          7.7676          6.7586
v  Pressure                -525.76          203.31          26.027          29.182
v  k                   9.9825e-011          8.2058          0.1698         0.34923
v  omega                    57.489     2.7322e+008     1.2912e+006           76900
v  TempK                    298.47          363.17          334.57          340.92
v  TurbVisc            2.5018e-018      0.00089211      4.157e-005       0.0001471
v  CourantNb            0.00014719          1.4916         0.79537         0.97607
v  FourierNb             0.0037528               1         0.40107         0.13764
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0032472     7.3128e-005      0.00019665

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.18          306.33
v  Yplus               0          2.9305         0.63492         0.49266


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59031          2.0817          1.1964          1.1137


 INSTANT    0.551000000E-02   TIME STEP NUMBER             551
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925191E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17474E-01 0.46823E+01
   Friction velocity        uk    :  0.17474E-01 0.46784E+01
   Dimensionless distance   yplus :  0.11848E-01 0.29304E+01
   Friction thermal sca.    tstar :  0.12111E+01 0.14469E+03
   Rough dim-less th. sca.  tplus :  0.83930E-02 0.20759E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27897E+00       9   0.68845E-05   0.21545E+01 0.23606E+02 
c  Velocity[X]                                      0.97299E+00 
c  Velocity[Y]                                      0.55462E+00 
c  Velocity[Z]                                      0.62686E+00 
c  Pressure     0.12188E-04      16   0.21946E-03   0.11948E-01 0.74754E+01 
c  k            0.13598E-01      11   0.19318E-04   0.31038E-01 0.41585E+02 
c  omega        0.27922E+07       1   0.62748E-07   0.76523E+07 0.44838E+00 
c  TempK        0.10067E+05       6   0.28081E-05   0.15872E+02 0.13903E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7038e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258          19.148      -0.0038038       -0.012363
v  Velocity[Y]             -15.502          14.901         0.15379         0.22329
v  Velocity[Z]             -25.567          12.223         -1.6599         -0.5088
v  ǁVelocityǁ         0.00022678          25.742          7.7673           6.758
v  Pressure                 -525.9          203.29          26.014          29.174
v  k                   9.9813e-011            8.72          0.1701         0.34999
v  omega                    57.489     2.7322e+008     1.2912e+006           76900
v  TempK                    298.47          363.17          334.59          340.96
v  TurbVisc            2.5015e-018      0.00089493     4.1646e-005      0.00014738
v  CourantNb            0.00014709          1.4917         0.79535         0.97606
v  FourierNb              0.003753               1         0.40114         0.13783
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0032209     7.3134e-005      0.00019669

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.19          306.33
v  Yplus               0          2.9304         0.63492         0.49264


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62387          2.0818          1.1965          1.1139


 INSTANT    0.552000000E-02   TIME STEP NUMBER             552
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925286E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17446E-01 0.46823E+01
   Friction velocity        uk    :  0.17446E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11829E-01 0.29302E+01
   Friction thermal sca.    tstar :  0.12109E+01 0.14482E+03
   Rough dim-less th. sca.  tplus :  0.83794E-02 0.20758E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27895E+00       9   0.69077E-05   0.21636E+01 0.23652E+02 
c  Velocity[X]                                      0.97824E+00 
c  Velocity[Y]                                      0.55724E+00 
c  Velocity[Z]                                      0.62816E+00 
c  Pressure     0.12846E-04      15   0.21193E-03   0.12590E-01 0.71600E+01 
c  k            0.13628E-01      11   0.19546E-04   0.31197E-01 0.41494E+02 
c  omega        0.27922E+07       1   0.61861E-07   0.58267E+07 0.39902E+00 
c  TempK        0.10067E+05       6   0.28004E-05   0.15786E+02 0.13863E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7032e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.147      -0.0038328       -0.012346
v  Velocity[Y]             -15.556          14.901         0.15407         0.22389
v  Velocity[Z]             -25.565          12.223         -1.6598        -0.50879
v  ǁVelocityǁ         0.00022954           25.74           7.767          6.7573
v  Pressure                -526.02          203.28          26.003          29.169
v  k                   9.9801e-011          8.5941          0.1704         0.35074
v  omega                    57.489     2.7322e+008     1.2912e+006           76901
v  TempK                    298.47          363.17           334.6          340.99
v  TurbVisc            2.5012e-018       0.0008976     4.1721e-005      0.00014766
v  CourantNb            0.00014696          1.4918         0.79533         0.97605
v  FourierNb             0.0037532               1         0.40121         0.13801
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0032375     7.3139e-005      0.00019672

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.19          306.33
v  Yplus               0          2.9302         0.63491         0.49263


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64946           2.082          1.1965          1.1141


 INSTANT    0.553000000E-02   TIME STEP NUMBER             553
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925360E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17415E-01 0.46823E+01
   Friction velocity        uk    :  0.17415E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11807E-01 0.29301E+01
   Friction thermal sca.    tstar :  0.12109E+01 0.14508E+03
   Rough dim-less th. sca.  tplus :  0.83644E-02 0.20757E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27893E+00       9   0.69296E-05   0.21767E+01 0.23741E+02 
c  Velocity[X]                                      0.98257E+00 
c  Velocity[Y]                                      0.56212E+00 
c  Velocity[Z]                                      0.63197E+00 
c  Pressure     0.12066E-04      15   0.22056E-03   0.11825E-01 0.75461E+01 
c  k            0.13657E-01      11   0.19717E-04   0.31440E-01 0.41517E+02 
c  omega        0.27922E+07       1   0.64672E-07   0.95041E+07 0.49103E+00 
c  TempK        0.10068E+05       6   0.27928E-05   0.15701E+02 0.13822E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7024e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.145      -0.0038571        -0.01233
v  Velocity[Y]              -15.62          14.901         0.15435         0.22448
v  Velocity[Z]             -25.564          12.223         -1.6597        -0.50877
v  ǁVelocityǁ         0.00023237          25.739          7.7667          6.7567
v  Pressure                -526.12          203.26          25.993          29.164
v  k                   9.9788e-011          8.3899          0.1707         0.35149
v  omega                    57.489     2.7322e+008     1.2912e+006           76901
v  TempK                    298.47          363.17          334.62          341.02
v  TurbVisc            2.5009e-018      0.00090011     4.1797e-005      0.00014794
v  CourantNb            0.00014683           1.492         0.79531         0.97603
v  FourierNb             0.0037536               1         0.40128         0.13819
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0032962     7.3144e-005      0.00019675

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.19          306.33
v  Yplus               0          2.9301         0.63491         0.49261


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51758          2.0822          1.1966          1.1142


 INSTANT    0.554000000E-02   TIME STEP NUMBER             554
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925306E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17365E-01 0.46823E+01
   Friction velocity        uk    :  0.17365E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11774E-01 0.29300E+01
   Friction thermal sca.    tstar :  0.12109E+01 0.14550E+03
   Rough dim-less th. sca.  tplus :  0.83405E-02 0.20756E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27892E+00       9   0.69676E-05   0.21923E+01 0.23817E+02 
c  Velocity[X]                                      0.98877E+00 
c  Velocity[Y]                                      0.56906E+00 
c  Velocity[Z]                                      0.63447E+00 
c  Pressure     0.12621E-04      15   0.21530E-03   0.12367E-01 0.73066E+01 
c  k            0.13687E-01      11   0.19959E-04   0.31664E-01 0.41501E+02 
c  omega        0.27922E+07       1   0.63957E-07   0.86381E+07 0.47797E+00 
c  TempK        0.10069E+05       6   0.27852E-05   0.15615E+02 0.13781E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7022e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.144      -0.0038818       -0.012311
v  Velocity[Y]             -15.593          14.901         0.15463         0.22507
v  Velocity[Z]             -25.562          12.224         -1.6596        -0.50876
v  ǁVelocityǁ         0.00023541          25.737          7.7663          6.7561
v  Pressure                -526.22          203.25          25.982          29.158
v  k                   9.9776e-011           8.211           0.171         0.35224
v  omega                    57.489     2.7322e+008     1.2912e+006           76901
v  TempK                    298.47          363.17          334.64          341.05
v  TurbVisc            2.5005e-018      0.00090246     4.1872e-005      0.00014822
v  CourantNb             0.0001467           1.492         0.79529         0.97602
v  FourierNb              0.003754               1         0.40135         0.13837
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0033199     7.3149e-005      0.00019678

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.19          306.34
v  Yplus               0            2.93          0.6349         0.49259


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.26765          2.0823          1.1966          1.1144


 INSTANT    0.555000000E-02   TIME STEP NUMBER             555
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925179E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17347E-01 0.46823E+01
   Friction velocity        uk    :  0.17347E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11761E-01 0.29298E+01
   Friction thermal sca.    tstar :  0.12109E+01 0.14565E+03
   Rough dim-less th. sca.  tplus :  0.83317E-02 0.20755E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27890E+00       9   0.70074E-05   0.21996E+01 0.23822E+02 
c  Velocity[X]                                      0.99240E+00 
c  Velocity[Y]                                      0.56928E+00 
c  Velocity[Z]                                      0.63792E+00 
c  Pressure     0.12156E-04      15   0.21922E-03   0.11911E-01 0.74034E+01 
c  k            0.13717E-01      11   0.20188E-04   0.31900E-01 0.41500E+02 
c  omega        0.27922E+07       1   0.64738E-07   0.90334E+07 0.48725E+00 
c  TempK        0.10069E+05       6   0.27775E-05   0.15528E+02 0.13739E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7023e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.143      -0.0039019       -0.012293
v  Velocity[Y]             -15.501          14.902         0.15491         0.22565
v  Velocity[Z]             -25.561          12.224         -1.6595        -0.50874
v  ǁVelocityǁ         0.00023796          25.736           7.766          6.7555
v  Pressure                -526.31          203.23          25.974          29.156
v  k                   9.9764e-011          8.5406         0.17129         0.35299
v  omega                    57.489     2.7322e+008     1.2912e+006           76901
v  TempK                    298.47          363.17          334.66          341.09
v  TurbVisc            2.5002e-018      0.00090465     4.1948e-005      0.00014851
v  CourantNb            0.00014655           1.492         0.79526         0.97601
v  FourierNb             0.0037545               1         0.40143         0.13855
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0033454     7.3154e-005      0.00019681

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.19          306.34
v  Yplus               0          2.9298         0.63489         0.49257


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35028          2.0824          1.1967          1.1146


 INSTANT    0.556000000E-02   TIME STEP NUMBER             556
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925197E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17339E-01 0.46823E+01
   Friction velocity        uk    :  0.17339E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11756E-01 0.29297E+01
   Friction thermal sca.    tstar :  0.12109E+01 0.14571E+03
   Rough dim-less th. sca.  tplus :  0.83283E-02 0.20754E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27888E+00       9   0.70573E-05   0.22120E+01 0.23882E+02 
c  Velocity[X]                                      0.99807E+00 
c  Velocity[Y]                                      0.57245E+00 
c  Velocity[Z]                                      0.64143E+00 
c  Pressure     0.12397E-04      15   0.21139E-03   0.12145E-01 0.75295E+01 
c  k            0.13746E-01      11   0.20499E-04   0.32213E-01 0.41582E+02 
c  omega        0.27922E+07       1   0.65696E-07   0.92814E+07 0.49372E+00 
c  TempK        0.10070E+05       6   0.27699E-05   0.15441E+02 0.13698E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7022e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.141      -0.0039222       -0.012272
v  Velocity[Y]             -15.473          14.902         0.15521         0.22624
v  Velocity[Z]             -25.559          12.224         -1.6594        -0.50873
v  ǁVelocityǁ         0.00024048          25.734          7.7657          6.7549
v  Pressure                -526.39          203.22          25.968          29.155
v  k                   9.9752e-011          9.0506         0.17159         0.35374
v  omega                    57.489     2.7322e+008     1.2912e+006           76901
v  TempK                    298.47          363.17          334.68          341.12
v  TurbVisc            2.4999e-018      0.00090684     4.2023e-005      0.00014879
v  CourantNb            0.00014645           1.492         0.79524         0.97599
v  FourierNb             0.0037548               1          0.4015         0.13874
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0033714     7.3159e-005      0.00019684

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.19          306.34
v  Yplus               0          2.9297         0.63489         0.49256


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52744          2.0825          1.1967          1.1147


 INSTANT    0.557000000E-02   TIME STEP NUMBER             557
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925145E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17318E-01 0.46823E+01
   Friction velocity        uk    :  0.17318E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11742E-01 0.29295E+01
   Friction thermal sca.    tstar :  0.12112E+01 0.14589E+03
   Rough dim-less th. sca.  tplus :  0.83179E-02 0.20753E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27886E+00       9   0.70911E-05   0.22267E+01 0.23969E+02 
c  Velocity[X]                                      0.10040E+01 
c  Velocity[Y]                                      0.57873E+00 
c  Velocity[Z]                                      0.64397E+00 
c  Pressure     0.12484E-04      16   0.21124E-03   0.12230E-01 0.74322E+01 
c  k            0.13776E-01      11   0.20705E-04   0.32347E-01 0.41476E+02 
c  omega        0.27922E+07       1   0.65525E-07   0.88626E+07 0.49175E+00 
c  TempK        0.10070E+05       6   0.27623E-05   0.15356E+02 0.13657E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7017e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257           19.14      -0.0039396       -0.012248
v  Velocity[Y]               -15.5          14.903          0.1555         0.22682
v  Velocity[Z]             -25.557          12.224         -1.6593        -0.50871
v  ǁVelocityǁ         0.00024323          25.732          7.7654          6.7542
v  Pressure                -526.46          203.21          25.958          29.151
v  k                    9.974e-011          8.9727         0.17189          0.3545
v  omega                    57.489     2.7322e+008     1.2912e+006           76901
v  TempK                    298.47          363.17           334.7          341.15
v  TurbVisc            2.4996e-018      0.00090965     4.2098e-005      0.00014907
v  CourantNb            0.00014634          1.4922         0.79523         0.97598
v  FourierNb              0.003755               1         0.40157         0.13892
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0033966     7.3164e-005      0.00019688

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.2          306.34
v  Yplus               0          2.9295         0.63488         0.49254


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51225          2.0826          1.1968          1.1149


 INSTANT    0.558000000E-02   TIME STEP NUMBER             558
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925158E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17294E-01 0.46823E+01
   Friction velocity        uk    :  0.17294E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11726E-01 0.29294E+01
   Friction thermal sca.    tstar :  0.12112E+01 0.14609E+03
   Rough dim-less th. sca.  tplus :  0.83066E-02 0.20752E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27884E+00       9   0.71156E-05   0.22335E+01 0.23972E+02 
c  Velocity[X]                                      0.10076E+01 
c  Velocity[Y]                                      0.57906E+00 
c  Velocity[Z]                                      0.64684E+00 
c  Pressure     0.12297E-04      15   0.21205E-03   0.12046E-01 0.73969E+01 
c  k            0.13805E-01      11   0.20979E-04   0.32541E-01 0.41466E+02 
c  omega        0.27922E+07       1   0.67742E-07   0.11887E+08 0.55771E+00 
c  TempK        0.10071E+05       6   0.27548E-05   0.15274E+02 0.13616E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.7007e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.139      -0.0039537        -0.01222
v  Velocity[Y]             -15.594          14.903         0.15579          0.2274
v  Velocity[Z]             -25.555          12.224         -1.6592        -0.50869
v  ǁVelocityǁ         0.00024587           25.73          7.7651          6.7536
v  Pressure                -526.52          203.19          25.948          29.146
v  k                   9.9728e-011          8.8197         0.17219         0.35525
v  omega                    57.489     2.7322e+008     1.2912e+006           76901
v  TempK                    298.47          363.17          334.71          341.18
v  TurbVisc            2.4993e-018      0.00092007     4.2173e-005      0.00014935
v  CourantNb            0.00014622          1.4924         0.79521         0.97596
v  FourierNb             0.0037552               1         0.40163          0.1391
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0034198     7.3169e-005      0.00019691

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.2          306.34
v  Yplus               0          2.9294         0.63488         0.49252


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5328          2.0829          1.1968          1.1151


 INSTANT    0.559000000E-02   TIME STEP NUMBER             559
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925245E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17259E-01 0.46823E+01
   Friction velocity        uk    :  0.17259E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11702E-01 0.29292E+01
   Friction thermal sca.    tstar :  0.12110E+01 0.14639E+03
   Rough dim-less th. sca.  tplus :  0.82898E-02 0.20751E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27882E+00       9   0.71469E-05   0.22476E+01 0.24041E+02 
c  Velocity[X]                                      0.10128E+01 
c  Velocity[Y]                                      0.58338E+00 
c  Velocity[Z]                                      0.65141E+00 
c  Pressure     0.12273E-04      16   0.21117E-03   0.12022E-01 0.74511E+01 
c  k            0.13835E-01      11   0.21282E-04   0.32762E-01 0.41490E+02 
c  omega        0.27922E+07       1   0.66888E-07   0.10430E+08 0.52888E+00 
c  TempK        0.10071E+05       5   0.52299E-05   0.14617E+02 0.13322E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6997e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.138      -0.0039644       -0.012191
v  Velocity[Y]             -15.653          14.903         0.15609         0.22798
v  Velocity[Z]             -25.553          12.225          -1.659        -0.50867
v  ǁVelocityǁ         0.00024862          25.728          7.7648           6.753
v  Pressure                -526.57          203.18          25.939          29.142
v  k                   9.9717e-011          8.5357         0.17248           0.356
v  omega                    57.489     2.7322e+008     1.2912e+006           76901
v  TempK                    298.47          363.17          334.73          341.21
v  TurbVisc             2.499e-018      0.00093329     4.2248e-005      0.00014964
v  CourantNb             0.0001461          1.4926         0.79519         0.97595
v  FourierNb             0.0037553               1          0.4017         0.13928
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006         0.00344     7.3173e-005      0.00019694

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.2          306.34
v  Yplus               0          2.9292         0.63487         0.49251


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56655          2.0832          1.1969          1.1152


 INSTANT    0.560000000E-02   TIME STEP NUMBER             560
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925255E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17218E-01 0.46823E+01
   Friction velocity        uk    :  0.17218E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11674E-01 0.29291E+01
   Friction thermal sca.    tstar :  0.12110E+01 0.14674E+03
   Rough dim-less th. sca.  tplus :  0.82698E-02 0.20750E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27880E+00       9   0.71889E-05   0.22590E+01 0.24109E+02 
c  Velocity[X]                                      0.10153E+01 
c  Velocity[Y]                                      0.58924E+00 
c  Velocity[Z]                                      0.65450E+00 
c  Pressure     0.12469E-04      15   0.21030E-03   0.12215E-01 0.75980E+01 
c  k            0.13864E-01      11   0.21492E-04   0.32919E-01 0.41448E+02 
c  omega        0.27922E+07       1   0.65953E-07   0.83290E+07 0.48917E+00 
c  TempK        0.10072E+05       5   0.52157E-05   0.14543E+02 0.13285E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6994e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.137      -0.0039759       -0.012161
v  Velocity[Y]              -15.58          14.903         0.15638         0.22855
v  Velocity[Z]             -25.552          12.225         -1.6589        -0.50866
v  ǁVelocityǁ         0.00025063          25.727          7.7644          6.7523
v  Pressure                -526.62          203.16          25.926          29.135
v  k                   9.9705e-011          8.3473         0.17278         0.35675
v  omega                    57.489     2.7322e+008     1.2912e+006           76901
v  TempK                    298.47          363.17          334.75          341.24
v  TurbVisc            2.4988e-018      0.00094687     4.2323e-005      0.00014992
v  CourantNb            0.00014599          1.4927         0.79517         0.97594
v  FourierNb             0.0037556               1         0.40177         0.13946
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0034571     7.3176e-005      0.00019697

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.2          306.34
v  Yplus               0          2.9291         0.63487         0.49249


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61933          2.0833          1.1969          1.1154


 INSTANT    0.561000000E-02   TIME STEP NUMBER             561
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925056E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17208E-01 0.46823E+01
   Friction velocity        uk    :  0.17208E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11667E-01 0.29290E+01
   Friction thermal sca.    tstar :  0.12111E+01 0.14682E+03
   Rough dim-less th. sca.  tplus :  0.82652E-02 0.20749E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27878E+00       9   0.72285E-05   0.22641E+01 0.24099E+02 
c  Velocity[X]                                      0.10196E+01 
c  Velocity[Y]                                      0.58755E+00 
c  Velocity[Z]                                      0.65693E+00 
c  Pressure     0.12725E-04      15   0.21301E-03   0.12465E-01 0.73225E+01 
c  k            0.13894E-01      11   0.21770E-04   0.33109E-01 0.41441E+02 
c  omega        0.27922E+07       1   0.63975E-07   0.42326E+07 0.38479E+00 
c  TempK        0.10072E+05       5   0.52015E-05   0.14470E+02 0.13248E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6993e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.136      -0.0039865       -0.012129
v  Velocity[Y]             -15.516          14.904         0.15667         0.22913
v  Velocity[Z]              -25.55          12.225         -1.6588        -0.50864
v  ǁVelocityǁ         0.00025337          25.725          7.7641          6.7517
v  Pressure                -526.66          203.15           25.92          29.135
v  k                   9.9693e-011           8.643         0.17307          0.3575
v  omega                    57.489     2.7322e+008     1.2912e+006           76901
v  TempK                    298.47          363.17          334.77          341.27
v  TurbVisc            2.4985e-018      0.00096073     4.2398e-005       0.0001502
v  CourantNb            0.00014591          1.4927         0.79515         0.97593
v  FourierNb             0.0037559               1         0.40184         0.13965
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0034632      7.318e-005        0.000197

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.2          306.34
v  Yplus               0           2.929         0.63486         0.49248


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54687          2.0834           1.197          1.1156


 INSTANT    0.562000000E-02   TIME STEP NUMBER             562
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925021E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17196E-01 0.46823E+01
   Friction velocity        uk    :  0.17196E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11659E-01 0.29288E+01
   Friction thermal sca.    tstar :  0.12110E+01 0.14692E+03
   Rough dim-less th. sca.  tplus :  0.82596E-02 0.20748E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27876E+00       9   0.72620E-05   0.22755E+01 0.24151E+02 
c  Velocity[X]                                      0.10249E+01 
c  Velocity[Y]                                      0.59032E+00 
c  Velocity[Z]                                      0.66028E+00 
c  Pressure     0.13118E-04      15   0.21847E-03   0.12850E-01 0.73208E+01 
c  k            0.13923E-01      11   0.22071E-04   0.33398E-01 0.41502E+02 
c  omega        0.27922E+07       1   0.65270E-07   0.60354E+07 0.43309E+00 
c  TempK        0.10073E+05       5   0.51873E-05   0.14397E+02 0.13210E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.699e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255          19.135      -0.0039962       -0.012097
v  Velocity[Y]             -15.501          14.904         0.15697         0.22969
v  Velocity[Z]             -25.549          12.225         -1.6586        -0.50862
v  ǁVelocityǁ         0.00025543          25.724          7.7638           6.751
v  Pressure                -526.69          203.14          25.913          29.133
v  k                   9.9682e-011          9.1108         0.17337         0.35824
v  omega                    57.489     2.7322e+008     1.2912e+006           76901
v  TempK                    298.47          363.17          334.79           341.3
v  TurbVisc            2.4982e-018      0.00097481     4.2473e-005      0.00015048
v  CourantNb            0.00014579          1.4928         0.79513         0.97591
v  FourierNb             0.0037564               1         0.40191         0.13983
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0034605     7.3184e-005      0.00019703

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.2          306.35
v  Yplus               0          2.9288         0.63485         0.49246


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42822          2.0835           1.197          1.1157


 INSTANT    0.563000000E-02   TIME STEP NUMBER             563
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924941E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17170E-01 0.46823E+01
   Friction velocity        uk    :  0.17170E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11642E-01 0.29287E+01
   Friction thermal sca.    tstar :  0.12111E+01 0.14715E+03
   Rough dim-less th. sca.  tplus :  0.82470E-02 0.20747E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27874E+00       9   0.73057E-05   0.22918E+01 0.24242E+02 
c  Velocity[X]                                      0.10308E+01 
c  Velocity[Y]                                      0.59403E+00 
c  Velocity[Z]                                      0.66701E+00 
c  Pressure     0.13264E-04      15   0.21509E-03   0.12994E-01 0.76852E+01 
c  k            0.13953E-01      11   0.22408E-04   0.33576E-01 0.41427E+02 
c  omega        0.27922E+07       1   0.68896E-07   0.11543E+08 0.55251E+00 
c  TempK        0.10073E+05       5   0.51732E-05   0.14324E+02 0.13174E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6984e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255          19.134      -0.0040036       -0.012062
v  Velocity[Y]             -15.555          14.905         0.15728         0.23026
v  Velocity[Z]             -25.547          12.225         -1.6585         -0.5086
v  ǁVelocityǁ         0.00025742          25.722          7.7634          6.7504
v  Pressure                -526.71          203.13           25.91          29.136
v  k                    9.967e-011          8.9823         0.17366         0.35899
v  omega                    57.489     2.7322e+008     1.2912e+006           76901
v  TempK                    298.48          363.17           334.8          341.33
v  TurbVisc            2.4979e-018      0.00098913     4.2548e-005      0.00015077
v  CourantNb            0.00014571          1.4929         0.79511          0.9759
v  FourierNb             0.0037568               1         0.40198         0.14001
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0034552     7.3187e-005      0.00019707

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.2          306.35
v  Yplus               0          2.9287         0.63485         0.49245


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44644          2.0837          1.1971          1.1159


 INSTANT    0.564000000E-02   TIME STEP NUMBER             564
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924847E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17141E-01 0.46823E+01
   Friction velocity        uk    :  0.17141E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11622E-01 0.29286E+01
   Friction thermal sca.    tstar :  0.12114E+01 0.14740E+03
   Rough dim-less th. sca.  tplus :  0.82330E-02 0.20746E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27872E+00       9   0.73546E-05   0.23129E+01 0.24376E+02 
c  Velocity[X]                                      0.10393E+01 
c  Velocity[Y]                                      0.60182E+00 
c  Velocity[Z]                                      0.67175E+00 
c  Pressure     0.13697E-04      15   0.21694E-03   0.13419E-01 0.75848E+01 
c  k            0.13982E-01      11   0.22663E-04   0.33878E-01 0.41481E+02 
c  omega        0.27922E+07       1   0.70889E-07   0.15180E+08 0.62385E+00 
c  TempK        0.10074E+05       5   0.51590E-05   0.14246E+02 0.13135E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6975e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255          19.133      -0.0040078       -0.012024
v  Velocity[Y]             -15.619          14.905         0.15758         0.23082
v  Velocity[Z]             -25.545          12.225         -1.6584        -0.50857
v  ǁVelocityǁ         0.00025948           25.72          7.7631          6.7497
v  Pressure                -526.72          203.12          25.908          29.139
v  k                   9.9659e-011          8.7223         0.17396         0.35974
v  omega                    57.489     2.7322e+008     1.2912e+006           76902
v  TempK                    298.48          363.17          334.82          341.36
v  TurbVisc            2.4976e-018       0.0010037     4.2623e-005      0.00015105
v  CourantNb            0.00014564          1.4931         0.79509         0.97589
v  FourierNb              0.003757               1         0.40205         0.14019
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.003402     7.3191e-005      0.00019709

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.21          306.35
v  Yplus               0          2.9286         0.63484         0.49243


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49338          2.0839          1.1971          1.1161


 INSTANT    0.565000000E-02   TIME STEP NUMBER             565
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924924E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17093E-01 0.46823E+01
   Friction velocity        uk    :  0.17093E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11589E-01 0.29284E+01
   Friction thermal sca.    tstar :  0.12113E+01 0.14781E+03
   Rough dim-less th. sca.  tplus :  0.82100E-02 0.20745E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27870E+00       9   0.73989E-05   0.23211E+01 0.24405E+02 
c  Velocity[X]                                      0.10426E+01 
c  Velocity[Y]                                      0.60455E+00 
c  Velocity[Z]                                      0.67396E+00 
c  Pressure     0.13714E-04      15   0.22115E-03   0.13436E-01 0.74705E+01 
c  k            0.14011E-01      11   0.22976E-04   0.34143E-01 0.41492E+02 
c  omega        0.27922E+07       1   0.69364E-07   0.13201E+08 0.59138E+00 
c  TempK        0.10074E+05       5   0.51448E-05   0.14165E+02 0.13096E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6973e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255          19.132      -0.0040121       -0.011985
v  Velocity[Y]             -15.592          14.905         0.15788         0.23138
v  Velocity[Z]             -25.543          12.225         -1.6583        -0.50855
v  ǁVelocityǁ         0.00026126          25.718          7.7628          6.7491
v  Pressure                -526.72          203.11          25.901          29.138
v  k                   9.9648e-011          8.4945         0.17425         0.36049
v  omega                    57.488     2.7322e+008     1.2912e+006           76902
v  TempK                    298.48          363.17          334.84          341.39
v  TurbVisc            2.4973e-018       0.0010184     4.2698e-005      0.00015133
v  CourantNb            0.00014555          1.4931         0.79506         0.97588
v  FourierNb             0.0037572               1         0.40212         0.14038
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0030636     7.3194e-005      0.00019712

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.21          306.35
v  Yplus               0          2.9284         0.63483         0.49241


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60771           2.084          1.1972          1.1163


 INSTANT    0.566000000E-02   TIME STEP NUMBER             566
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925195E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17076E-01 0.46823E+01
   Friction velocity        uk    :  0.17076E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11578E-01 0.29283E+01
   Friction thermal sca.    tstar :  0.12111E+01 0.14796E+03
   Rough dim-less th. sca.  tplus :  0.82017E-02 0.20744E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27868E+00       9   0.74328E-05   0.23239E+01 0.24392E+02 
c  Velocity[X]                                      0.10446E+01 
c  Velocity[Y]                                      0.60279E+00 
c  Velocity[Z]                                      0.67658E+00 
c  Pressure     0.13392E-04      16   0.22811E-03   0.13122E-01 0.81106E+01 
c  k            0.14041E-01      11   0.23492E-04   0.34379E-01 0.41506E+02 
c  omega        0.27922E+07       1   0.66208E-07   0.73346E+07 0.46336E+00 
c  TempK        0.10075E+05       5   0.51307E-05   0.14083E+02 0.13056E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6974e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.254          19.132      -0.0040138       -0.011941
v  Velocity[Y]             -15.501          14.905         0.15819         0.23194
v  Velocity[Z]             -25.541          12.225         -1.6581        -0.50853
v  ǁVelocityǁ         0.00026276          25.716          7.7624          6.7485
v  Pressure                -526.74          203.09          25.883          29.126
v  k                   9.9636e-011          8.7852         0.17454         0.36124
v  omega                    57.488     2.7322e+008     1.2912e+006           76902
v  TempK                    298.48          363.17          334.86          341.42
v  TurbVisc             2.497e-018       0.0010333     4.2773e-005      0.00015162
v  CourantNb            0.00014549          1.4931         0.79504         0.97586
v  FourierNb             0.0037574               1         0.40219         0.14056
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0029586     7.3198e-005      0.00019715

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.21          306.35
v  Yplus               0          2.9283         0.63482         0.49239


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65048          2.0841          1.1972          1.1164


 INSTANT    0.567000000E-02   TIME STEP NUMBER             567
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925196E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17066E-01 0.46822E+01
   Friction velocity        uk    :  0.17066E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11571E-01 0.29281E+01
   Friction thermal sca.    tstar :  0.12112E+01 0.14805E+03
   Rough dim-less th. sca.  tplus :  0.81970E-02 0.20743E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27865E+00       9   0.74552E-05   0.23295E+01 0.24408E+02 
c  Velocity[X]                                      0.10472E+01 
c  Velocity[Y]                                      0.60325E+00 
c  Velocity[Z]                                      0.67909E+00 
c  Pressure     0.12903E-04      15   0.21789E-03   0.12645E-01 0.74484E+01 
c  k            0.14070E-01      11   0.23652E-04   0.34723E-01 0.41611E+02 
c  omega        0.27922E+07       1   0.64482E-07   0.39851E+07 0.37851E+00 
c  TempK        0.10075E+05       5   0.51167E-05   0.14004E+02 0.13018E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6972e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.254          19.131      -0.0040134       -0.011895
v  Velocity[Y]             -15.475          14.906          0.1585          0.2325
v  Velocity[Z]              -25.54          12.225          -1.658        -0.50851
v  ǁVelocityǁ         0.00026498          25.715          7.7621          6.7478
v  Pressure                -526.73          203.08          25.876          29.125
v  k                   9.9625e-011          9.2624         0.17484         0.36198
v  omega                    57.488     2.7322e+008     1.2912e+006           76902
v  TempK                    298.48          363.17          334.87          341.45
v  TurbVisc            2.4967e-018       0.0010483     4.2848e-005       0.0001519
v  CourantNb            0.00014543          1.4932         0.79502         0.97585
v  FourierNb             0.0037576               1         0.40226         0.14074
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0029147     7.3201e-005      0.00019718

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.21          306.35
v  Yplus               0          2.9281         0.63481         0.49238


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66478          2.0841          1.1973          1.1166


 INSTANT    0.568000000E-02   TIME STEP NUMBER             568
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925258E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17042E-01 0.46822E+01
   Friction velocity        uk    :  0.17042E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11555E-01 0.29280E+01
   Friction thermal sca.    tstar :  0.12112E+01 0.14825E+03
   Rough dim-less th. sca.  tplus :  0.81854E-02 0.20742E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27863E+00       9   0.74907E-05   0.23357E+01 0.24436E+02 
c  Velocity[X]                                      0.10500E+01 
c  Velocity[Y]                                      0.60429E+00 
c  Velocity[Z]                                      0.68143E+00 
c  Pressure     0.12586E-04      15   0.21817E-03   0.12336E-01 0.74282E+01 
c  k            0.14099E-01      11   0.24212E-04   0.34917E-01 0.41557E+02 
c  omega        0.27922E+07       1   0.64298E-07   0.37620E+07 0.36862E+00 
c  TempK        0.10076E+05       5   0.51027E-05   0.13929E+02 0.12981E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6967e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.254           19.13      -0.0040096       -0.011846
v  Velocity[Y]             -15.502          14.906         0.15882         0.23305
v  Velocity[Z]             -25.538          12.225         -1.6578        -0.50849
v  ǁVelocityǁ         0.00026619          25.713          7.7618          6.7472
v  Pressure                -526.72          203.06          25.869          29.123
v  k                   9.9614e-011          9.1618         0.17513         0.36273
v  omega                    57.488     2.7322e+008     1.2912e+006           76902
v  TempK                    298.48          363.17          334.89          341.48
v  TurbVisc            2.4965e-018       0.0010634     4.2922e-005      0.00015218
v  CourantNb            0.00014533          1.4933           0.795         0.97584
v  FourierNb             0.0037579               1         0.40233         0.14092
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0028706     7.3205e-005      0.00019721

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.21          306.35
v  Yplus               0           2.928          0.6348         0.49236


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58216          2.0843          1.1973          1.1168


 INSTANT    0.569000000E-02   TIME STEP NUMBER             569
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925283E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17019E-01 0.46822E+01
   Friction velocity        uk    :  0.17019E-01 0.46783E+01
   Dimensionless distance   yplus :  0.11539E-01 0.29279E+01
   Friction thermal sca.    tstar :  0.12112E+01 0.14845E+03
   Rough dim-less th. sca.  tplus :  0.81745E-02 0.20742E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27861E+00       9   0.75405E-05   0.23450E+01 0.24483E+02 
c  Velocity[X]                                      0.10539E+01 
c  Velocity[Y]                                      0.60582E+00 
c  Velocity[Z]                                      0.68531E+00 
c  Pressure     0.12685E-04      15   0.21419E-03   0.12438E-01 0.74214E+01 
c  k            0.14128E-01      11   0.24739E-04   0.35156E-01 0.41585E+02 
c  omega        0.27922E+07       1   0.67851E-07   0.96630E+07 0.50899E+00 
c  TempK        0.10076E+05       5   0.50888E-05   0.13852E+02 0.12944E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6958e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.129      -0.0040014       -0.011795
v  Velocity[Y]             -15.596          14.906         0.15913          0.2336
v  Velocity[Z]             -25.537          12.225         -1.6577        -0.50846
v  ǁVelocityǁ         0.00026792          25.712          7.7614          6.7465
v  Pressure                -526.69          203.05          25.863          29.123
v  k                   9.9603e-011          8.9688         0.17542         0.36347
v  omega                    57.488     2.7322e+008     1.2912e+006           76902
v  TempK                    298.48          363.17          334.91          341.51
v  TurbVisc            2.4962e-018       0.0010785     4.2997e-005      0.00015247
v  CourantNb             0.0001453          1.4935         0.79498         0.97583
v  FourierNb             0.0037582               1          0.4024          0.1411
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.002826     7.3209e-005      0.00019724

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.21          306.35
v  Yplus               0          2.9279         0.63479         0.49234


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56303          2.0845          1.1974          1.1169


 INSTANT    0.570000000E-02   TIME STEP NUMBER             570
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925134E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16982E-01 0.46822E+01
   Friction velocity        uk    :  0.16982E-01 0.46782E+01
   Dimensionless distance   yplus :  0.11514E-01 0.29278E+01
   Friction thermal sca.    tstar :  0.12112E+01 0.14878E+03
   Rough dim-less th. sca.  tplus :  0.81568E-02 0.20741E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27858E+00       9   0.76856E-05   0.23616E+01 0.24587E+02 
c  Velocity[X]                                      0.10598E+01 
c  Velocity[Y]                                      0.61037E+00 
c  Velocity[Z]                                      0.69151E+00 
c  Pressure     0.13017E-04      15   0.21308E-03   0.12767E-01 0.78408E+01 
c  k            0.14157E-01      11   0.25375E-04   0.35485E-01 0.41681E+02 
c  omega        0.27922E+07       1   0.70836E-07   0.15328E+08 0.61516E+00 
c  TempK        0.10077E+05       5   0.50749E-05   0.13774E+02 0.12907E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6949e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.129      -0.0039868       -0.011739
v  Velocity[Y]             -15.655          14.907         0.15945         0.23415
v  Velocity[Z]             -25.535          12.225         -1.6575        -0.50844
v  ǁVelocityǁ         0.00026876           25.71          7.7611          6.7459
v  Pressure                -526.66          203.05          25.861          29.126
v  k                   9.9593e-011          8.6467         0.17571         0.36421
v  omega                    57.488     2.7322e+008     1.2912e+006           76902
v  TempK                    298.48          363.17          334.92          341.54
v  TurbVisc            2.4959e-018       0.0010934     4.3071e-005      0.00015275
v  CourantNb            0.00014522          1.4937         0.79496         0.97581
v  FourierNb             0.0037586               1         0.40247         0.14129
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0028791     7.3212e-005      0.00019727

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.22          306.36
v  Yplus               0          2.9278         0.63478         0.49232


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52183          2.0848          1.1974          1.1171


 INSTANT    0.571000000E-02   TIME STEP NUMBER             571
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924846E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16942E-01 0.46822E+01
   Friction velocity        uk    :  0.16942E-01 0.46782E+01
   Dimensionless distance   yplus :  0.11487E-01 0.29276E+01
   Friction thermal sca.    tstar :  0.12115E+01 0.14913E+03
   Rough dim-less th. sca.  tplus :  0.81376E-02 0.20740E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27856E+00       9   0.77566E-05   0.23791E+01 0.24696E+02 
c  Velocity[X]                                      0.10658E+01 
c  Velocity[Y]                                      0.61806E+00 
c  Velocity[Z]                                      0.69521E+00 
c  Pressure     0.12908E-04      15   0.21069E-03   0.12666E-01 0.76182E+01 
c  k            0.14185E-01      11   0.25748E-04   0.35843E-01 0.41779E+02 
c  omega        0.27922E+07       1   0.69317E-07   0.13106E+08 0.57713E+00 
c  TempK        0.10077E+05       5   0.50610E-05   0.13697E+02 0.12867E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6947e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.128       -0.003968       -0.011682
v  Velocity[Y]             -15.581          14.907         0.15977          0.2347
v  Velocity[Z]             -25.533          12.225         -1.6574        -0.50842
v  ǁVelocityǁ         0.00026973          25.708          7.7607          6.7453
v  Pressure                -526.62          203.04          25.858          29.129
v  k                   9.9582e-011          8.4013         0.17599         0.36495
v  omega                    57.488     2.7322e+008     1.2912e+006           76902
v  TempK                    298.48          363.17          334.94          341.57
v  TurbVisc            2.4956e-018        0.001108     4.3145e-005      0.00015303
v  CourantNb             0.0001452          1.4937         0.79494          0.9758
v  FourierNb             0.0037589               1         0.40253         0.14146
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0028846     7.3214e-005       0.0001973

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.22          306.36
v  Yplus               0          2.9276         0.63477          0.4923


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58946          2.0849          1.1975          1.1173


 INSTANT    0.572000000E-02   TIME STEP NUMBER             572
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924893E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16933E-01 0.46822E+01
   Friction velocity        uk    :  0.16933E-01 0.46782E+01
   Dimensionless distance   yplus :  0.11481E-01 0.29275E+01
   Friction thermal sca.    tstar :  0.12114E+01 0.14921E+03
   Rough dim-less th. sca.  tplus :  0.81331E-02 0.20739E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27854E+00       9   0.77944E-05   0.23787E+01 0.24628E+02 
c  Velocity[X]                                      0.10688E+01 
c  Velocity[Y]                                      0.61307E+00 
c  Velocity[Z]                                      0.69691E+00 
c  Pressure     0.12776E-04      15   0.20864E-03   0.12542E-01 0.75642E+01 
c  k            0.14214E-01      11   0.25612E-04   0.36245E-01 0.41903E+02 
c  omega        0.27922E+07       1   0.66543E-07   0.81131E+07 0.46963E+00 
c  TempK        0.10077E+05       5   0.50472E-05   0.13618E+02 0.12829E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6947e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.252          19.127      -0.0039445       -0.011623
v  Velocity[Y]             -15.518          14.907          0.1601         0.23525
v  Velocity[Z]             -25.532          12.224         -1.6572        -0.50839
v  ǁVelocityǁ         0.00026991          25.707          7.7604          6.7446
v  Pressure                -526.59          203.03          25.852          29.128
v  k                   9.9571e-011          8.6701         0.17628         0.36568
v  omega                    57.488     2.7322e+008     1.2912e+006           76902
v  TempK                    298.48          363.17          334.96           341.6
v  TurbVisc            2.4954e-018       0.0011224     4.3219e-005      0.00015332
v  CourantNb            0.00014517          1.4937         0.79492         0.97579
v  FourierNb             0.0037591               1          0.4026         0.14164
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0028899     7.3217e-005      0.00019732

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.22          306.36
v  Yplus               0          2.9275         0.63476         0.49228


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65957           2.085          1.1975          1.1174


 INSTANT    0.573000000E-02   TIME STEP NUMBER             573
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925110E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16920E-01 0.46822E+01
   Friction velocity        uk    :  0.16920E-01 0.46782E+01
   Dimensionless distance   yplus :  0.11472E-01 0.29274E+01
   Friction thermal sca.    tstar :  0.12112E+01 0.14932E+03
   Rough dim-less th. sca.  tplus :  0.81270E-02 0.20738E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27851E+00       9   0.78007E-05   0.23866E+01 0.24659E+02 
c  Velocity[X]                                      0.10723E+01 
c  Velocity[Y]                                      0.61394E+00 
c  Velocity[Z]                                      0.70039E+00 
c  Pressure     0.12805E-04      15   0.20731E-03   0.12575E-01 0.74781E+01 
c  k            0.14243E-01      11   0.26043E-04   0.36699E-01 0.42067E+02 
c  omega        0.27922E+07       1   0.63905E-07   0.38426E+07 0.35349E+00 
c  TempK        0.10078E+05       5   0.50334E-05   0.13540E+02 0.12790E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6944e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.252          19.127      -0.0039171       -0.011565
v  Velocity[Y]             -15.503          14.908         0.16043          0.2358
v  Velocity[Z]              -25.53          12.224         -1.6571        -0.50836
v  ǁVelocityǁ          0.0002709          25.705            7.76           6.744
v  Pressure                -526.55          203.02          25.843          29.125
v  k                   9.9561e-011          9.1182         0.17657         0.36641
v  omega                    57.488     2.7322e+008     1.2912e+006           76902
v  TempK                    298.48          363.17          334.97          341.63
v  TurbVisc            2.4951e-018       0.0011365     4.3293e-005       0.0001536
v  CourantNb            0.00014518          1.4938          0.7949         0.97578
v  FourierNb             0.0037593               1         0.40267         0.14182
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0028954      7.322e-005      0.00019735

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.22          306.36
v  Yplus               0          2.9274         0.63474         0.49226


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82096           2.085          1.1976          1.1176


 INSTANT    0.574000000E-02   TIME STEP NUMBER             574
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925245E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16893E-01 0.46822E+01
   Friction velocity        uk    :  0.16893E-01 0.46782E+01
   Dimensionless distance   yplus :  0.11454E-01 0.29273E+01
   Friction thermal sca.    tstar :  0.12112E+01 0.14956E+03
   Rough dim-less th. sca.  tplus :  0.81139E-02 0.20737E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27849E+00       9   0.77571E-05   0.23952E+01 0.24710E+02 
c  Velocity[X]                                      0.10745E+01 
c  Velocity[Y]                                      0.61611E+00 
c  Velocity[Z]                                      0.70460E+00 
c  Pressure     0.12858E-04      15   0.20753E-03   0.12634E-01 0.74671E+01 
c  k            0.14271E-01      11   0.26458E-04   0.37001E-01 0.42081E+02 
c  omega        0.27922E+07       1   0.65014E-07   0.58585E+07 0.41017E+00 
c  TempK        0.10078E+05       5   0.50195E-05   0.13462E+02 0.12752E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6939e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.252          19.126      -0.0038854       -0.011504
v  Velocity[Y]             -15.557          14.908         0.16076         0.23635
v  Velocity[Z]             -25.529          12.224         -1.6569        -0.50834
v  ǁVelocityǁ          0.0002716          25.703          7.7596          6.7434
v  Pressure                 -526.5             203          25.834          29.122
v  k                    9.955e-011          8.9791         0.17685         0.36714
v  omega                    57.488     2.7322e+008     1.2912e+006           76902
v  TempK                    298.48          363.17          334.99          341.66
v  TurbVisc            2.4948e-018       0.0011501     4.3366e-005      0.00015388
v  CourantNb            0.00014513          1.4939         0.79487         0.97577
v  FourierNb             0.0037595               1         0.40274           0.142
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0029008     7.3223e-005      0.00019738

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.22          306.36
v  Yplus               0          2.9273         0.63473         0.49224


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.84422          2.0852          1.1976          1.1178


 INSTANT    0.575000000E-02   TIME STEP NUMBER             575
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925255E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16858E-01 0.46822E+01
   Friction velocity        uk    :  0.16858E-01 0.46782E+01
   Dimensionless distance   yplus :  0.11430E-01 0.29272E+01
   Friction thermal sca.    tstar :  0.12113E+01 0.14988E+03
   Rough dim-less th. sca.  tplus :  0.80970E-02 0.20736E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27846E+00       9   0.78019E-05   0.24075E+01 0.24787E+02 
c  Velocity[X]                                      0.10772E+01 
c  Velocity[Y]                                      0.62030E+00 
c  Velocity[Z]                                      0.71002E+00 
c  Pressure     0.12765E-04      15   0.20317E-03   0.12547E-01 0.74593E+01 
c  k            0.14299E-01      11   0.26751E-04   0.37331E-01 0.42181E+02 
c  omega        0.27922E+07       1   0.67383E-07   0.95215E+07 0.49500E+00 
c  TempK        0.10079E+05       5   0.50058E-05   0.13385E+02 0.12714E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6931e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.251          19.126      -0.0038478       -0.011441
v  Velocity[Y]             -15.621          14.908         0.16109         0.23689
v  Velocity[Z]             -25.527          12.224         -1.6568        -0.50831
v  ǁVelocityǁ         0.00027206          25.702          7.7593          6.7427
v  Pressure                -526.44          202.99          25.828          29.122
v  k                    9.954e-011          8.6988         0.17713         0.36787
v  omega                    57.488     2.7322e+008     1.2912e+006           76902
v  TempK                    298.49          363.17          335.01          341.69
v  TurbVisc            2.4946e-018       0.0011631     4.3439e-005      0.00015416
v  CourantNb             0.0001451          1.4941         0.79485         0.97576
v  FourierNb             0.0037597               1         0.40281         0.14217
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0029063     7.3227e-005       0.0001974

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.22          306.36
v  Yplus               0          2.9272         0.63472         0.49222


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76269          2.0854          1.1977          1.1179


 INSTANT    0.576000000E-02   TIME STEP NUMBER             576
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925131E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16808E-01 0.46822E+01
   Friction velocity        uk    :  0.16808E-01 0.46782E+01
   Dimensionless distance   yplus :  0.11396E-01 0.29271E+01
   Friction thermal sca.    tstar :  0.12112E+01 0.15032E+03
   Rough dim-less th. sca.  tplus :  0.80732E-02 0.20736E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27844E+00       9   0.78507E-05   0.24214E+01 0.24862E+02 
c  Velocity[X]                                      0.10815E+01 
c  Velocity[Y]                                      0.62612E+00 
c  Velocity[Z]                                      0.71382E+00 
c  Pressure     0.12989E-04      15   0.20645E-03   0.12774E-01 0.73267E+01 
c  k            0.14328E-01      11   0.26935E-04   0.37617E-01 0.42233E+02 
c  omega        0.27922E+07       1   0.67576E-07   0.10549E+08 0.51888E+00 
c  TempK        0.10079E+05       5   0.49920E-05   0.13310E+02 0.12677E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6931e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.251          19.125      -0.0038064       -0.011376
v  Velocity[Y]             -15.594          14.908         0.16142         0.23743
v  Velocity[Z]             -25.526          12.224         -1.6566        -0.50829
v  ǁVelocityǁ         0.00027232          25.701          7.7589          6.7421
v  Pressure                -526.37          202.98          25.824          29.122
v  k                    9.953e-011          8.4337         0.17741          0.3686
v  omega                    57.488     2.7322e+008     1.2912e+006           76902
v  TempK                    298.49          363.17          335.03          341.72
v  TurbVisc            2.4943e-018       0.0011756     4.3512e-005      0.00015444
v  CourantNb            0.00014508          1.4941         0.79483         0.97575
v  FourierNb               0.00376               1         0.40287         0.14235
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0031727      7.323e-005      0.00019743

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.22          306.36
v  Yplus               0          2.9271          0.6347         0.49219


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61466          2.0855          1.1977          1.1181


 INSTANT    0.577000000E-02   TIME STEP NUMBER             577
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925089E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16788E-01 0.46822E+01
   Friction velocity        uk    :  0.16788E-01 0.46782E+01
   Dimensionless distance   yplus :  0.11382E-01 0.29270E+01
   Friction thermal sca.    tstar :  0.12112E+01 0.15050E+03
   Rough dim-less th. sca.  tplus :  0.80634E-02 0.20735E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27841E+00       9   0.78963E-05   0.24344E+01 0.24911E+02 
c  Velocity[X]                                      0.10870E+01 
c  Velocity[Y]                                      0.62771E+00 
c  Velocity[Z]                                      0.71970E+00 
c  Pressure     0.12728E-04      16   0.20903E-03   0.12523E-01 0.77152E+01 
c  k            0.14356E-01      11   0.27237E-04   0.37858E-01 0.42265E+02 
c  omega        0.27922E+07       1   0.68898E-07   0.12204E+08 0.55027E+00 
c  TempK        0.10079E+05       5   0.49784E-05   0.13237E+02 0.12640E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6933e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.251          19.124      -0.0037601       -0.011308
v  Velocity[Y]             -15.503          14.909         0.16177         0.23797
v  Velocity[Z]             -25.524          12.223         -1.6565        -0.50827
v  ǁVelocityǁ         0.00027179          25.699          7.7586          6.7415
v  Pressure                -526.31          202.97          25.819          29.124
v  k                    9.952e-011           8.717         0.17769         0.36932
v  omega                    57.488     2.7322e+008     1.2912e+006           76902
v  TempK                    298.49          363.17          335.04          341.75
v  TurbVisc            2.4941e-018       0.0011873     4.3584e-005      0.00015472
v  CourantNb            0.00014507           1.494         0.79481         0.97574
v  FourierNb             0.0037602               1         0.40294         0.14253
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006         0.00349     7.3233e-005      0.00019745

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.23          306.36
v  Yplus               0           2.927         0.63469         0.49217


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66201          2.0855          1.1978          1.1183


 INSTANT    0.578000000E-02   TIME STEP NUMBER             578
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925084E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16781E-01 0.46822E+01
   Friction velocity        uk    :  0.16781E-01 0.46782E+01
   Dimensionless distance   yplus :  0.11378E-01 0.29268E+01
   Friction thermal sca.    tstar :  0.12115E+01 0.15056E+03
   Rough dim-less th. sca.  tplus :  0.80602E-02 0.20734E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27839E+00       9   0.79389E-05   0.24493E+01 0.24992E+02 
c  Velocity[X]                                      0.10931E+01 
c  Velocity[Y]                                      0.63294E+00 
c  Velocity[Z]                                      0.72327E+00 
c  Pressure     0.12418E-04      16   0.21459E-03   0.12223E-01 0.74620E+01 
c  k            0.14384E-01      11   0.27498E-04   0.38177E-01 0.42369E+02 
c  omega        0.27922E+07       1   0.66577E-07   0.86959E+07 0.47452E+00 
c  TempK        0.10080E+05       5   0.49648E-05   0.13159E+02 0.12603E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6933e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.25          19.124      -0.0037084       -0.011239
v  Velocity[Y]             -15.476          14.909         0.16212         0.23851
v  Velocity[Z]             -25.523          12.223         -1.6563        -0.50824
v  ǁVelocityǁ         0.00027148          25.697          7.7582          6.7409
v  Pressure                -526.24          202.95          25.812          29.122
v  k                    9.951e-011          9.1427         0.17797         0.37004
v  omega                    57.488     2.7322e+008     1.2912e+006           76902
v  TempK                    298.49          363.17          335.06          341.78
v  TurbVisc            2.4938e-018       0.0011984     4.3657e-005        0.000155
v  CourantNb           5.8017e-005           1.494         0.79479         0.97573
v  FourierNb             0.0037605               1         0.40301          0.1427
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0035079     7.3237e-005      0.00019748

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.23          306.36
v  Yplus               0          2.9268         0.63467         0.49215


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.80068          2.0855          1.1978          1.1184


 INSTANT    0.579000000E-02   TIME STEP NUMBER             579
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925261E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16755E-01 0.46822E+01
   Friction velocity        uk    :  0.16755E-01 0.46782E+01
   Dimensionless distance   yplus :  0.11360E-01 0.29267E+01
   Friction thermal sca.    tstar :  0.12115E+01 0.15080E+03
   Rough dim-less th. sca.  tplus :  0.80475E-02 0.20733E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27836E+00       9   0.79856E-05   0.24581E+01 0.25001E+02 
c  Velocity[X]                                      0.10971E+01 
c  Velocity[Y]                                      0.63342E+00 
c  Velocity[Z]                                      0.72765E+00 
c  Pressure     0.12175E-04      16   0.21247E-03   0.11988E-01 0.76377E+01 
c  k            0.14412E-01      11   0.27673E-04   0.38361E-01 0.42350E+02 
c  omega        0.27922E+07       1   0.65770E-07   0.74914E+07 0.44634E+00 
c  TempK        0.10080E+05       5   0.49513E-05   0.13082E+02 0.12565E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6929e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.25          19.123      -0.0036533       -0.011168
v  Velocity[Y]             -15.503          14.909         0.16247         0.23906
v  Velocity[Z]             -25.521          12.223         -1.6561        -0.50822
v  ǁVelocityǁ         0.00027105          25.696          7.7579          6.7403
v  Pressure                -526.18          202.93          25.798          29.114
v  k                     9.95e-011          9.0266         0.17825         0.37076
v  omega                    57.487     2.7322e+008     1.2912e+006           76902
v  TempK                    298.49          363.17          335.08           341.8
v  TurbVisc            2.4936e-018       0.0012088     4.3729e-005      0.00015528
v  CourantNb           4.6216e-005          1.4941         0.79477         0.97572
v  FourierNb             0.0037608               1         0.40308         0.14287
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0038587     7.3241e-005      0.00019751

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.23          306.37
v  Yplus               0          2.9267         0.63466         0.49213


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69596          2.0856          1.1978          1.1186


 INSTANT    0.580000000E-02   TIME STEP NUMBER             580
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925398E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16728E-01 0.46821E+01
   Friction velocity        uk    :  0.16728E-01 0.46782E+01
   Dimensionless distance   yplus :  0.11342E-01 0.29266E+01
   Friction thermal sca.    tstar :  0.12113E+01 0.15104E+03
   Rough dim-less th. sca.  tplus :  0.80348E-02 0.20732E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27834E+00       9   0.80257E-05   0.24720E+01 0.25055E+02 
c  Velocity[X]                                      0.11030E+01 
c  Velocity[Y]                                      0.63565E+00 
c  Velocity[Z]                                      0.73338E+00 
c  Pressure     0.12359E-04      15   0.21406E-03   0.12173E-01 0.75378E+01 
c  k            0.14439E-01      11   0.27797E-04   0.38561E-01 0.42377E+02 
c  omega        0.27922E+07       1   0.65377E-07   0.68115E+07 0.42407E+00 
c  TempK        0.10081E+05       5   0.49378E-05   0.13007E+02 0.12529E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6921e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.25          19.123      -0.0035944       -0.011095
v  Velocity[Y]              -15.58           14.91         0.16282          0.2396
v  Velocity[Z]             -25.519          12.222          -1.656        -0.50819
v  ǁVelocityǁ         0.00027005          25.694          7.7575          6.7397
v  Pressure                 -526.1          202.92          25.787          29.108
v  k                    9.949e-011          8.8372         0.17853         0.37147
v  omega                    57.487     2.7322e+008     1.2912e+006           76902
v  TempK                    298.49          363.17          335.09          341.83
v  TurbVisc            2.4933e-018       0.0012184       4.38e-005      0.00015556
v  CourantNb            0.00013972          1.4943         0.79475         0.97571
v  FourierNb              0.003761               1         0.40314         0.14305
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0042445     7.3244e-005      0.00019753

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.23          306.37
v  Yplus               0          2.9266         0.63464         0.49211


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64328          2.0859          1.1979          1.1188


 INSTANT    0.581000000E-02   TIME STEP NUMBER             581
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925265E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16693E-01 0.46821E+01
   Friction velocity        uk    :  0.16693E-01 0.46781E+01
   Dimensionless distance   yplus :  0.11318E-01 0.29265E+01
   Friction thermal sca.    tstar :  0.12113E+01 0.15136E+03
   Rough dim-less th. sca.  tplus :  0.80178E-02 0.20731E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27831E+00       9   0.80710E-05   0.24884E+01 0.25146E+02 
c  Velocity[X]                                      0.11076E+01 
c  Velocity[Y]                                      0.64006E+00 
c  Velocity[Z]                                      0.74075E+00 
c  Pressure     0.12420E-04      15   0.21252E-03   0.12238E-01 0.74577E+01 
c  k            0.14467E-01      11   0.27861E-04   0.38780E-01 0.42435E+02 
c  omega        0.27922E+07       1   0.66748E-07   0.87492E+07 0.46944E+00 
c  TempK        0.10081E+05       5   0.49243E-05   0.12934E+02 0.12493E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6913e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.249          19.123      -0.0035301        -0.01102
v  Velocity[Y]             -15.647           14.91         0.16318         0.24013
v  Velocity[Z]             -25.518          12.222         -1.6558        -0.50816
v  ǁVelocityǁ         0.00026977          25.693          7.7572          6.7391
v  Pressure                -526.01           202.9           25.78          29.106
v  k                   9.9481e-011          8.5297          0.1788         0.37219
v  omega                    57.487     2.7322e+008     1.2912e+006           76902
v  TempK                    298.49          363.17          335.11          341.86
v  TurbVisc            2.4931e-018       0.0012272     4.3872e-005      0.00015584
v  CourantNb            0.00014519          1.4945         0.79473          0.9757
v  FourierNb             0.0037612               1         0.40321         0.14322
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0044577     7.3247e-005      0.00019756

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.23          306.37
v  Yplus               0          2.9265         0.63463         0.49208


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58827          2.0861          1.1979          1.1189


 INSTANT    0.582000000E-02   TIME STEP NUMBER             582
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925076E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16646E-01 0.46821E+01
   Friction velocity        uk    :  0.16646E-01 0.46781E+01
   Dimensionless distance   yplus :  0.11286E-01 0.29264E+01
   Friction thermal sca.    tstar :  0.12113E+01 0.15178E+03
   Rough dim-less th. sca.  tplus :  0.79952E-02 0.20731E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27829E+00       9   0.81173E-05   0.25034E+01 0.25246E+02 
c  Velocity[X]                                      0.11114E+01 
c  Velocity[Y]                                      0.64687E+00 
c  Velocity[Z]                                      0.74511E+00 
c  Pressure     0.12332E-04      15   0.21081E-03   0.12155E-01 0.73731E+01 
c  k            0.14494E-01      11   0.27915E-04   0.38933E-01 0.42447E+02 
c  omega        0.27922E+07       1   0.65992E-07   0.83463E+07 0.46273E+00 
c  TempK        0.10081E+05       5   0.49108E-05   0.12862E+02 0.12456E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6912e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.249          19.122       -0.003462       -0.010946
v  Velocity[Y]             -15.611           14.91         0.16354         0.24067
v  Velocity[Z]             -25.516          12.222         -1.6557        -0.50813
v  ǁVelocityǁ         0.00026829          25.691          7.7568          6.7385
v  Pressure                -525.92          202.89          25.774          29.106
v  k                   9.9471e-011          8.2177         0.17908          0.3729
v  omega                    57.487     2.7322e+008     1.2912e+006           76902
v  TempK                    298.49          363.17          335.12          341.89
v  TurbVisc            2.4928e-018        0.001235     4.3942e-005      0.00015611
v  CourantNb            0.00014519          1.4945         0.79471          0.9757
v  FourierNb             0.0037614               1         0.40328         0.14339
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0044836     7.3251e-005      0.00019758

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.23          306.37
v  Yplus               0          2.9264         0.63462         0.49206


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55843          2.0861           1.198          1.1191


 INSTANT    0.583000000E-02   TIME STEP NUMBER             583
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925046E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16623E-01 0.46821E+01
   Friction velocity        uk    :  0.16623E-01 0.46781E+01
   Dimensionless distance   yplus :  0.11270E-01 0.29263E+01
   Friction thermal sca.    tstar :  0.12113E+01 0.15200E+03
   Rough dim-less th. sca.  tplus :  0.79841E-02 0.20730E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27826E+00       9   0.81627E-05   0.25148E+01 0.25274E+02 
c  Velocity[X]                                      0.11167E+01 
c  Velocity[Y]                                      0.64712E+00 
c  Velocity[Z]                                      0.75090E+00 
c  Pressure     0.12164E-04      15   0.20997E-03   0.11993E-01 0.74882E+01 
c  k            0.14522E-01      11   0.28295E-04   0.39013E-01 0.42415E+02 
c  omega        0.27922E+07       1   0.66518E-07   0.89973E+07 0.47404E+00 
c  TempK        0.10082E+05       5   0.48973E-05   0.12790E+02 0.12420E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6914e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.249          19.122      -0.0033892        -0.01087
v  Velocity[Y]             -15.511           14.91          0.1639         0.24121
v  Velocity[Z]             -25.515          12.221         -1.6555        -0.50811
v  ǁVelocityǁ         0.00026711           25.69          7.7565          6.7379
v  Pressure                -525.83          202.88          25.765          29.103
v  k                   9.9462e-011          8.4379         0.17935          0.3736
v  omega                    57.487     2.7322e+008     1.2912e+006           76902
v  TempK                    298.49          363.17          335.14          341.92
v  TurbVisc            2.4926e-018       0.0012418     4.4013e-005      0.00015639
v  CourantNb            0.00014526          1.4944         0.79469         0.97569
v  FourierNb             0.0037616               1         0.40334         0.14356
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0044694     7.3254e-005       0.0001976

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.23          306.37
v  Yplus               0          2.9263          0.6346         0.49203


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60675          2.0861           1.198          1.1193


 INSTANT    0.584000000E-02   TIME STEP NUMBER             584
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925092E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16614E-01 0.46821E+01
   Friction velocity        uk    :  0.16613E-01 0.46781E+01
   Dimensionless distance   yplus :  0.11264E-01 0.29262E+01
   Friction thermal sca.    tstar :  0.12113E+01 0.15208E+03
   Rough dim-less th. sca.  tplus :  0.79797E-02 0.20729E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27824E+00       9   0.81980E-05   0.25316E+01 0.25361E+02 
c  Velocity[X]                                      0.11237E+01 
c  Velocity[Y]                                      0.65060E+00 
c  Velocity[Z]                                      0.75729E+00 
c  Pressure     0.12214E-04      15   0.21468E-03   0.12046E-01 0.76890E+01 
c  k            0.14549E-01      11   0.28124E-04   0.39159E-01 0.42454E+02 
c  omega        0.27922E+07       1   0.66890E-07   0.89281E+07 0.46818E+00 
c  TempK        0.10082E+05       5   0.48839E-05   0.12718E+02 0.12385E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6914e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.248          19.121      -0.0033127       -0.010795
v  Velocity[Y]             -15.478          14.911         0.16427         0.24175
v  Velocity[Z]             -25.513          12.221         -1.6554        -0.50809
v  ǁVelocityǁ         0.00026531          25.688          7.7562          6.7374
v  Pressure                -525.74          202.86          25.758          29.101
v  k                   9.9453e-011          8.8115         0.17962         0.37431
v  omega                    57.487     2.7322e+008     1.2912e+006           76902
v  TempK                     298.5          363.17          335.16          341.95
v  TurbVisc            2.4924e-018       0.0012478     4.4083e-005      0.00015666
v  CourantNb             0.0001453          1.4944         0.79467         0.97568
v  FourierNb             0.0037618               1         0.40341         0.14373
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0044083     7.3258e-005      0.00019763

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.24          306.37
v  Yplus               0          2.9262         0.63458           0.492


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66322          2.0862          1.1981          1.1194


 INSTANT    0.585000000E-02   TIME STEP NUMBER             585
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925066E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16587E-01 0.46821E+01
   Friction velocity        uk    :  0.16587E-01 0.46781E+01
   Dimensionless distance   yplus :  0.11246E-01 0.29260E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.15232E+03
   Rough dim-less th. sca.  tplus :  0.79670E-02 0.20728E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27821E+00       9   0.82316E-05   0.25508E+01 0.25471E+02 
c  Velocity[X]                                      0.11319E+01 
c  Velocity[Y]                                      0.65742E+00 
c  Velocity[Z]                                      0.76145E+00 
c  Pressure     0.12297E-04      15   0.21891E-03   0.12131E-01 0.75342E+01 
c  k            0.14576E-01      11   0.27847E-04   0.39159E-01 0.42398E+02 
c  omega        0.27922E+07       1   0.66246E-07   0.83492E+07 0.45722E+00 
c  TempK        0.10083E+05       5   0.48705E-05   0.12644E+02 0.12348E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6911e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.248          19.121      -0.0032312       -0.010719
v  Velocity[Y]             -15.502          14.911         0.16464         0.24228
v  Velocity[Z]             -25.512           12.22         -1.6552        -0.50807
v  ǁVelocityǁ         0.00026381          25.686          7.7558          6.7368
v  Pressure                -525.65          202.85          25.749          29.097
v  k                   9.9444e-011           8.711         0.17989         0.37501
v  omega                    57.487     2.7322e+008     1.2912e+006           76902
v  TempK                     298.5          363.17          335.17          341.98
v  TurbVisc            2.4921e-018        0.001253     4.4153e-005      0.00015694
v  CourantNb            0.00014538          1.4945         0.79465         0.97568
v  FourierNb              0.003762               1         0.40347          0.1439
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0043422     7.3261e-005      0.00019765

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.24          306.37
v  Yplus               0           2.926         0.63456         0.49197


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66598          2.0863          1.1981          1.1196


 INSTANT    0.586000000E-02   TIME STEP NUMBER             586
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925143E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16560E-01 0.46821E+01
   Friction velocity        uk    :  0.16560E-01 0.46781E+01
   Dimensionless distance   yplus :  0.11228E-01 0.29259E+01
   Friction thermal sca.    tstar :  0.12115E+01 0.15257E+03
   Rough dim-less th. sca.  tplus :  0.79541E-02 0.20727E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27819E+00       9   0.82566E-05   0.25630E+01 0.25507E+02 
c  Velocity[X]                                      0.11378E+01 
c  Velocity[Y]                                      0.65830E+00 
c  Velocity[Z]                                      0.76694E+00 
c  Pressure     0.12328E-04      15   0.21759E-03   0.12165E-01 0.76960E+01 
c  k            0.14603E-01      11   0.27868E-04   0.39160E-01 0.42376E+02 
c  omega        0.27922E+07       1   0.68064E-07   0.11403E+08 0.52402E+00 
c  TempK        0.10083E+05       5   0.48571E-05   0.12568E+02 0.12311E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6905e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.248           19.12      -0.0031486       -0.010644
v  Velocity[Y]             -15.595          14.911         0.16501         0.24282
v  Velocity[Z]              -25.51           12.22          -1.655        -0.50804
v  ǁVelocityǁ         0.00026189          25.685          7.7555          6.7362
v  Pressure                -525.55          202.83          25.735          29.089
v  k                   9.9435e-011          8.5246         0.18016         0.37571
v  omega                    57.487     2.7322e+008     1.2912e+006           76902
v  TempK                     298.5          363.17          335.19             342
v  TurbVisc            2.4919e-018       0.0012574     4.4222e-005      0.00015721
v  CourantNb            0.00014544          1.4947         0.79462         0.97567
v  FourierNb             0.0037622               1         0.40353         0.14406
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0042699     7.3265e-005      0.00019767

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.24          306.37
v  Yplus               0          2.9259         0.63454         0.49194


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53622          2.0865          1.1982          1.1197


 INSTANT    0.587000000E-02   TIME STEP NUMBER             587
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925235E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16521E-01 0.46820E+01
   Friction velocity        uk    :  0.16521E-01 0.46781E+01
   Dimensionless distance   yplus :  0.11202E-01 0.29258E+01
   Friction thermal sca.    tstar :  0.12113E+01 0.15293E+03
   Rough dim-less th. sca.  tplus :  0.79353E-02 0.20727E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27816E+00       9   0.82814E-05   0.25796E+01 0.25597E+02 
c  Velocity[X]                                      0.11443E+01 
c  Velocity[Y]                                      0.66246E+00 
c  Velocity[Z]                                      0.77290E+00 
c  Pressure     0.12227E-04      15   0.21433E-03   0.12068E-01 0.75309E+01 
c  k            0.14630E-01      11   0.27827E-04   0.39214E-01 0.42391E+02 
c  omega        0.27922E+07       1   0.66612E-07   0.95636E+07 0.48093E+00 
c  TempK        0.10084E+05       5   0.48438E-05   0.12495E+02 0.12274E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6897e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.248           19.12       -0.003064        -0.01057
v  Velocity[Y]             -15.654          14.911         0.16538         0.24335
v  Velocity[Z]             -25.508          12.219         -1.6549        -0.50802
v  ǁVelocityǁ         0.00026057          25.683          7.7552          6.7357
v  Pressure                -525.44          202.81          25.726          29.085
v  k                   9.9426e-011          8.2114         0.18043          0.3764
v  omega                    57.487     2.7322e+008     1.2912e+006           76902
v  TempK                     298.5          363.17          335.21          342.03
v  TurbVisc            2.4917e-018        0.001261     4.4291e-005      0.00015748
v  CourantNb            0.00014552          1.4948          0.7946         0.97567
v  FourierNb             0.0037624               1          0.4036         0.14423
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0041914     7.3268e-005      0.00019769

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.24          306.38
v  Yplus               0          2.9258         0.63452         0.49191


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.597          2.0867          1.1982          1.1199


 INSTANT    0.588000000E-02   TIME STEP NUMBER             588
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925249E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16477E-01 0.46820E+01
   Friction velocity        uk    :  0.16477E-01 0.46781E+01
   Dimensionless distance   yplus :  0.11172E-01 0.29257E+01
   Friction thermal sca.    tstar :  0.12114E+01 0.15334E+03
   Rough dim-less th. sca.  tplus :  0.79140E-02 0.20726E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27814E+00       9   0.83113E-05   0.25964E+01 0.25687E+02 
c  Velocity[X]                                      0.11507E+01 
c  Velocity[Y]                                      0.66792E+00 
c  Velocity[Z]                                      0.77770E+00 
c  Pressure     0.12338E-04      15   0.21644E-03   0.12181E-01 0.78033E+01 
c  k            0.14657E-01      11   0.27621E-04   0.39181E-01 0.42345E+02 
c  omega        0.27922E+07       1   0.65432E-07   0.73888E+07 0.43253E+00 
c  TempK        0.10084E+05       5   0.48306E-05   0.12423E+02 0.12238E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6897e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.247           19.12      -0.0029784       -0.010495
v  Velocity[Y]             -15.583          14.912         0.16576         0.24388
v  Velocity[Z]             -25.507          12.219         -1.6547        -0.50799
v  ǁVelocityǁ         0.00025791          25.682          7.7548          6.7351
v  Pressure                -525.34          202.79          25.711          29.076
v  k                   9.9417e-011          7.9438          0.1807          0.3771
v  omega                    57.487     2.7322e+008     1.2912e+006           76902
v  TempK                     298.5          363.17          335.22          342.06
v  TurbVisc            2.4915e-018       0.0012638      4.436e-005      0.00015775
v  CourantNb            0.00014555          1.4948         0.79458         0.97566
v  FourierNb             0.0037626               1         0.40366         0.14439
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.004098     7.3272e-005      0.00019772

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.24          306.38
v  Yplus               0          2.9257          0.6345         0.49188


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49356          2.0867          1.1982          1.1201


 INSTANT    0.589000000E-02   TIME STEP NUMBER             589
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925240E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16461E-01 0.46820E+01
   Friction velocity        uk    :  0.16461E-01 0.46780E+01
   Dimensionless distance   yplus :  0.11161E-01 0.29256E+01
   Friction thermal sca.    tstar :  0.12114E+01 0.16026E+03
   Rough dim-less th. sca.  tplus :  0.79065E-02 0.20725E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27811E+00       9   0.83489E-05   0.26044E+01 0.25696E+02 
c  Velocity[X]                                      0.11551E+01 
c  Velocity[Y]                                      0.66658E+00 
c  Velocity[Z]                                      0.78265E+00 
c  Pressure     0.12619E-04      15   0.21357E-03   0.12461E-01 0.79054E+01 
c  k            0.14684E-01      11   0.27499E-04   0.39107E-01 0.42285E+02 
c  omega        0.27922E+07       1   0.63356E-07   0.34902E+07 0.31486E+00 
c  TempK        0.10084E+05       5   0.48176E-05   0.12353E+02 0.12202E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6899e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.247          19.119      -0.0028885       -0.010417
v  Velocity[Y]             -15.522          14.912         0.16613         0.24442
v  Velocity[Z]             -25.505          12.218         -1.6546        -0.50796
v  ǁVelocityǁ         0.00025552           25.68          7.7545          6.7345
v  Pressure                -525.24          202.77          25.695          29.066
v  k                   9.9409e-011            8.23         0.18096         0.37779
v  omega                    57.487     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17          335.24          342.09
v  TurbVisc            2.4913e-018       0.0012652     4.4428e-005      0.00015802
v  CourantNb            0.00014567          1.4948         0.79456         0.97566
v  FourierNb             0.0037628               1         0.40373         0.14456
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0039997     7.3275e-005      0.00019774

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.24          306.38
v  Yplus               0          2.9256         0.63448         0.49184


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49905          2.0867          1.1983          1.1202


 INSTANT    0.590000000E-02   TIME STEP NUMBER             590
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925127E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16443E-01 0.46820E+01
   Friction velocity        uk    :  0.16443E-01 0.46780E+01
   Dimensionless distance   yplus :  0.11149E-01 0.29255E+01
   Friction thermal sca.    tstar :  0.12114E+01 0.18733E+03
   Rough dim-less th. sca.  tplus :  0.78978E-02 0.20725E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27809E+00       9   0.83624E-05   0.26149E+01 0.25750E+02 
c  Velocity[X]                                      0.11581E+01 
c  Velocity[Y]                                      0.66862E+00 
c  Velocity[Z]                                      0.78823E+00 
c  Pressure     0.12512E-04      15   0.20903E-03   0.12359E-01 0.75823E+01 
c  k            0.14711E-01      11   0.27277E-04   0.39069E-01 0.42264E+02 
c  omega        0.27922E+07       1   0.64462E-07   0.52106E+07 0.36979E+00 
c  TempK        0.10085E+05       5   0.48045E-05   0.12283E+02 0.12166E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6899e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.247          19.119      -0.0027944       -0.010339
v  Velocity[Y]             -15.508          14.912         0.16651         0.24495
v  Velocity[Z]             -25.504          12.218         -1.6544        -0.50794
v  ǁVelocityǁ         0.00025291          25.679          7.7542           6.734
v  Pressure                -525.13          202.75          25.686          29.061
v  k                     9.94e-011          8.6655         0.18123         0.37847
v  omega                    57.487     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17          335.25          342.11
v  TurbVisc             2.491e-018       0.0012659     4.4496e-005      0.00015829
v  CourantNb            0.00014576          1.4948         0.79454         0.97565
v  FourierNb              0.003763               1         0.40379         0.14472
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0038922     7.3278e-005      0.00019776

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.24          306.38
v  Yplus               0          2.9255         0.63446         0.49181


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42534          2.0867          1.1983          1.1204


 INSTANT    0.591000000E-02   TIME STEP NUMBER             591
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925123E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16415E-01 0.46820E+01
   Friction velocity        uk    :  0.16415E-01 0.46780E+01
   Dimensionless distance   yplus :  0.11129E-01 0.29254E+01
   Friction thermal sca.    tstar :  0.12114E+01 0.20193E+03
   Rough dim-less th. sca.  tplus :  0.78841E-02 0.20724E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27806E+00       9   0.83760E-05   0.26275E+01 0.25832E+02 
c  Velocity[X]                                      0.11597E+01 
c  Velocity[Y]                                      0.67208E+00 
c  Velocity[Z]                                      0.79574E+00 
c  Pressure     0.12420E-04      15   0.20878E-03   0.12272E-01 0.78365E+01 
c  k            0.14737E-01      11   0.27091E-04   0.38870E-01 0.42118E+02 
c  omega        0.27922E+07       1   0.68089E-07   0.10913E+08 0.50880E+00 
c  TempK        0.10085E+05       5   0.47915E-05   0.12214E+02 0.12131E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6896e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.247          19.119      -0.0026956        -0.01026
v  Velocity[Y]             -15.563          14.912         0.16689         0.24548
v  Velocity[Z]             -25.502          12.217         -1.6543        -0.50792
v  ǁVelocityǁ         0.00025046          25.677          7.7539          6.7334
v  Pressure                -525.01          202.74           25.68           29.06
v  k                   9.9392e-011          8.5256         0.18149         0.37916
v  omega                    57.486     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17          335.27          342.14
v  TurbVisc            2.4908e-018       0.0012665     4.4564e-005      0.00015856
v  CourantNb            0.00014587          1.4949         0.79452         0.97565
v  FourierNb             0.0037632               1         0.40385         0.14488
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.003995      7.328e-005      0.00019777

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.25          306.38
v  Yplus               0          2.9254         0.63444         0.49178


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35431          2.0869          1.1984          1.1205


 INSTANT    0.592000000E-02   TIME STEP NUMBER             592
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925117E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16379E-01 0.46820E+01
   Friction velocity        uk    :  0.16378E-01 0.46780E+01
   Dimensionless distance   yplus :  0.11105E-01 0.29253E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.18306E+03
   Rough dim-less th. sca.  tplus :  0.78668E-02 0.20723E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27803E+00       9   0.84125E-05   0.26437E+01 0.25948E+02 
c  Velocity[X]                                      0.11624E+01 
c  Velocity[Y]                                      0.67957E+00 
c  Velocity[Z]                                      0.80172E+00 
c  Pressure     0.12417E-04      15   0.20874E-03   0.12273E-01 0.78110E+01 
c  k            0.14763E-01      11   0.26803E-04   0.38742E-01 0.42042E+02 
c  omega        0.27922E+07       1   0.69966E-07   0.14189E+08 0.57578E+00 
c  TempK        0.10086E+05       5   0.47785E-05   0.12143E+02 0.12095E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.689e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.246          19.118        -0.00259       -0.010182
v  Velocity[Y]             -15.626          14.912         0.16727         0.24601
v  Velocity[Z]               -25.5          12.216         -1.6542         -0.5079
v  ǁVelocityǁ         0.00024754          25.675          7.7535          6.7329
v  Pressure                -524.89          202.73          25.671          29.056
v  k                   9.9384e-011          8.2479         0.18176         0.37984
v  omega                    57.486     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17          335.29          342.17
v  TurbVisc            2.4906e-018       0.0012668     4.4632e-005      0.00015882
v  CourantNb            0.00014596           1.495          0.7945         0.97565
v  FourierNb             0.0037633               1         0.40391         0.14504
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040674     7.3281e-005      0.00019779

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.25          306.38
v  Yplus               0          2.9253         0.63442         0.49175


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51796           2.087          1.1984          1.1207


 INSTANT    0.593000000E-02   TIME STEP NUMBER             593
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925303E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16329E-01 0.46819E+01
   Friction velocity        uk    :  0.16329E-01 0.46780E+01
   Dimensionless distance   yplus :  0.11071E-01 0.29252E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.15698E+03
   Rough dim-less th. sca.  tplus :  0.78428E-02 0.20722E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27801E+00       9   0.84215E-05   0.26505E+01 0.25968E+02 
c  Velocity[X]                                      0.11631E+01 
c  Velocity[Y]                                      0.68202E+00 
c  Velocity[Z]                                      0.80545E+00 
c  Pressure     0.12508E-04      15   0.20805E-03   0.12367E-01 0.79566E+01 
c  k            0.14790E-01      11   0.26552E-04   0.38581E-01 0.41932E+02 
c  omega        0.27922E+07       1   0.68468E-07   0.12236E+08 0.54215E+00 
c  TempK        0.10086E+05       5   0.47657E-05   0.12071E+02 0.12058E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6891e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.246          19.118      -0.0024835       -0.010105
v  Velocity[Y]             -15.596          14.912         0.16765         0.24654
v  Velocity[Z]             -25.499          12.216          -1.654        -0.50787
v  ǁVelocityǁ         0.00024467          25.674          7.7532          6.7323
v  Pressure                -524.78          202.71          25.655          29.046
v  k                   9.9376e-011          7.9566         0.18202         0.38051
v  omega                    57.486     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17           335.3           342.2
v  TurbVisc            2.4904e-018        0.001267     4.4699e-005      0.00015909
v  CourantNb            0.00014608           1.495         0.79448         0.97564
v  FourierNb             0.0037635               1         0.40397          0.1452
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.004155     7.3283e-005      0.00019781

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.25          306.38
v  Yplus               0          2.9252          0.6344         0.49172


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63773           2.087          1.1985          1.1208


 INSTANT    0.594000000E-02   TIME STEP NUMBER             594
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925298E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16303E-01 0.46819E+01
   Friction velocity        uk    :  0.16303E-01 0.46779E+01
   Dimensionless distance   yplus :  0.11054E-01 0.29251E+01
   Friction thermal sca.    tstar :  0.12114E+01 0.15498E+03
   Rough dim-less th. sca.  tplus :  0.78306E-02 0.20721E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27798E+00       9   0.84445E-05   0.26554E+01 0.25961E+02 
c  Velocity[X]                                      0.11642E+01 
c  Velocity[Y]                                      0.68069E+00 
c  Velocity[Z]                                      0.81056E+00 
c  Pressure     0.12638E-04      15   0.21219E-03   0.12500E-01 0.81217E+01 
c  k            0.14816E-01      11   0.26234E-04   0.38362E-01 0.41785E+02 
c  omega        0.27922E+07       1   0.65539E-07   0.69445E+07 0.41934E+00 
c  TempK        0.10086E+05       5   0.47529E-05   0.12001E+02 0.12022E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6895e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.246          19.117      -0.0023745       -0.010029
v  Velocity[Y]             -15.504          14.913         0.16803         0.24707
v  Velocity[Z]             -25.497          12.215         -1.6539        -0.50785
v  ǁVelocityǁ         0.00024136          25.672          7.7529          6.7318
v  Pressure                -524.68          202.68          25.636          29.033
v  k                   9.9368e-011          8.1981         0.18228         0.38118
v  omega                    57.486     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17          335.32          342.22
v  TurbVisc            2.4902e-018       0.0012661     4.4765e-005      0.00015935
v  CourantNb             0.0001462          1.4949         0.79446         0.97564
v  FourierNb             0.0037637               1         0.40404         0.14535
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0042153     7.3284e-005      0.00019782

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.25          306.38
v  Yplus               0          2.9251         0.63437         0.49168


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65656           2.087          1.1985           1.121


 INSTANT    0.595000000E-02   TIME STEP NUMBER             595
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925213E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16290E-01 0.46819E+01
   Friction velocity        uk    :  0.16290E-01 0.46779E+01
   Dimensionless distance   yplus :  0.11045E-01 0.29250E+01
   Friction thermal sca.    tstar :  0.12115E+01 0.15510E+03
   Rough dim-less th. sca.  tplus :  0.78244E-02 0.20721E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27796E+00       9   0.84641E-05   0.26643E+01 0.25981E+02 
c  Velocity[X]                                      0.11667E+01 
c  Velocity[Y]                                      0.68174E+00 
c  Velocity[Z]                                      0.81584E+00 
c  Pressure     0.12670E-04      15   0.21742E-03   0.12535E-01 0.78494E+01 
c  k            0.14842E-01      11   0.25877E-04   0.38245E-01 0.41710E+02 
c  omega        0.27922E+07       1   0.63658E-07   0.34884E+07 0.31859E+00 
c  TempK        0.10087E+05       5   0.47403E-05   0.11931E+02 0.11986E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6897e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.246          19.117      -0.0022655      -0.0099558
v  Velocity[Y]             -15.476          14.913         0.16841          0.2476
v  Velocity[Z]             -25.495          12.215         -1.6537        -0.50782
v  ǁVelocityǁ          0.0002388           25.67          7.7526          6.7313
v  Pressure                -524.56          202.66          25.622          29.025
v  k                    9.936e-011          8.5808         0.18254         0.38185
v  omega                    57.486     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17          335.33          342.25
v  TurbVisc              2.49e-018       0.0012647     4.4831e-005      0.00015962
v  CourantNb            0.00014633          1.4948         0.79444         0.97563
v  FourierNb             0.0037639               1          0.4041          0.1455
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0037915     7.3285e-005      0.00019783

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.25          306.38
v  Yplus               0           2.925         0.63435         0.49165


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67147           2.087          1.1985          1.1211


 INSTANT    0.596000000E-02   TIME STEP NUMBER             596
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925217E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16264E-01 0.46819E+01
   Friction velocity        uk    :  0.16264E-01 0.46779E+01
   Dimensionless distance   yplus :  0.11027E-01 0.29249E+01
   Friction thermal sca.    tstar :  0.12115E+01 0.15535E+03
   Rough dim-less th. sca.  tplus :  0.78116E-02 0.20720E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27793E+00       9   0.84807E-05   0.26750E+01 0.26019E+02 
c  Velocity[X]                                      0.11700E+01 
c  Velocity[Y]                                      0.68357E+00 
c  Velocity[Z]                                      0.82147E+00 
c  Pressure     0.12569E-04      15   0.21221E-03   0.12439E-01 0.78702E+01 
c  k            0.14868E-01      11   0.25708E-04   0.38012E-01 0.41545E+02 
c  omega        0.27922E+07       1   0.63696E-07   0.32847E+07 0.31415E+00 
c  TempK        0.10087E+05       5   0.47276E-05   0.11863E+02 0.11951E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6895e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.246          19.117      -0.0021551      -0.0098828
v  Velocity[Y]             -15.502          14.913         0.16879         0.24813
v  Velocity[Z]             -25.494          12.215         -1.6536         -0.5078
v  ǁVelocityǁ         0.00023513          25.669          7.7523          6.7307
v  Pressure                -524.45          202.64          25.608          29.016
v  k                   9.9353e-011          8.4684          0.1828         0.38252
v  omega                    57.486     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17          335.35          342.28
v  TurbVisc            2.4898e-018        0.001263     4.4897e-005      0.00015988
v  CourantNb            0.00014642          1.4949         0.79442         0.97563
v  FourierNb             0.0037641               1         0.40416         0.14566
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.003974     7.3285e-005      0.00019785

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.25          306.39
v  Yplus               0          2.9249         0.63433         0.49162


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68135           2.087          1.1986          1.1213


 INSTANT    0.597000000E-02   TIME STEP NUMBER             597
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925236E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16236E-01 0.46818E+01
   Friction velocity        uk    :  0.16235E-01 0.46779E+01
   Dimensionless distance   yplus :  0.11008E-01 0.29248E+01
   Friction thermal sca.    tstar :  0.12115E+01 0.15562E+03
   Rough dim-less th. sca.  tplus :  0.77981E-02 0.20719E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27791E+00       9   0.85015E-05   0.26841E+01 0.26057E+02 
c  Velocity[X]                                      0.11711E+01 
c  Velocity[Y]                                      0.68502E+00 
c  Velocity[Z]                                      0.82799E+00 
c  Pressure     0.12589E-04      15   0.21464E-03   0.12463E-01 0.78002E+01 
c  k            0.14893E-01      11   0.25353E-04   0.37789E-01 0.41409E+02 
c  omega        0.27922E+07       1   0.67100E-07   0.86175E+07 0.46274E+00 
c  TempK        0.10088E+05       5   0.47150E-05   0.11797E+02 0.11917E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6889e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.246          19.116       -0.002045       -0.009811
v  Velocity[Y]             -15.577          14.913         0.16917         0.24866
v  Velocity[Z]             -25.492          12.216         -1.6535        -0.50778
v  ǁVelocityǁ         0.00023214          25.668          7.7519          6.7302
v  Pressure                -524.34          202.63          25.596          29.009
v  k                   9.9345e-011          8.2866         0.18306         0.38318
v  omega                    57.486     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17          335.36          342.31
v  TurbVisc            2.4896e-018       0.0012639     4.4963e-005      0.00016014
v  CourantNb            0.00014658           1.495         0.79441         0.97562
v  FourierNb             0.0037643               1         0.40422         0.14581
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040598     7.3286e-005      0.00019786

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.25          306.39
v  Yplus               0          2.9248         0.63432         0.49159


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66093          2.0872          1.1986          1.1214


 INSTANT    0.598000000E-02   TIME STEP NUMBER             598
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925259E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16200E-01 0.46818E+01
   Friction velocity        uk    :  0.16200E-01 0.46778E+01
   Dimensionless distance   yplus :  0.10984E-01 0.29247E+01
   Friction thermal sca.    tstar :  0.12115E+01 0.15597E+03
   Rough dim-less th. sca.  tplus :  0.77808E-02 0.20719E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27788E+00       9   0.86315E-05   0.26972E+01 0.26142E+02 
c  Velocity[X]                                      0.11708E+01 
c  Velocity[Y]                                      0.68899E+00 
c  Velocity[Z]                                      0.83741E+00 
c  Pressure     0.12508E-04      15   0.21829E-03   0.12386E-01 0.81451E+01 
c  k            0.14919E-01      11   0.25070E-04   0.37630E-01 0.41306E+02 
c  omega        0.27922E+07       1   0.70815E-07   0.13969E+08 0.57307E+00 
c  TempK        0.10088E+05       5   0.47026E-05   0.11735E+02 0.11885E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6883e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.245          19.116      -0.0019339       -0.009742
v  Velocity[Y]             -15.645          14.913         0.16956         0.24918
v  Velocity[Z]             -25.491          12.216         -1.6534        -0.50775
v  ǁVelocityǁ         0.00022887          25.666          7.7516          6.7297
v  Pressure                -524.21          202.61          25.587          29.005
v  k                   9.9338e-011          7.9887         0.18332         0.38384
v  omega                    57.486     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17          335.38          342.33
v  TurbVisc            2.4895e-018        0.001273     4.5028e-005       0.0001604
v  CourantNb            0.00014669          1.4952         0.79438         0.97562
v  FourierNb             0.0037644               1         0.40428         0.14596
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040587     7.3286e-005      0.00019787

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.26          306.39
v  Yplus               0          2.9247          0.6343         0.49157


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52471          2.0874          1.1987          1.1216


 INSTANT    0.599000000E-02   TIME STEP NUMBER             599
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925230E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16151E-01 0.46818E+01
   Friction velocity        uk    :  0.16151E-01 0.46778E+01
   Dimensionless distance   yplus :  0.10951E-01 0.29246E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.15644E+03
   Rough dim-less th. sca.  tplus :  0.77575E-02 0.20718E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27786E+00       9   0.86803E-05   0.27144E+01 0.26247E+02 
c  Velocity[X]                                      0.11747E+01 
c  Velocity[Y]                                      0.69747E+00 
c  Velocity[Z]                                      0.84221E+00 
c  Pressure     0.12963E-04      15   0.22074E-03   0.12842E-01 0.82247E+01 
c  k            0.14945E-01      11   0.24850E-04   0.37505E-01 0.41185E+02 
c  omega        0.27922E+07       1   0.69900E-07   0.13286E+08 0.56703E+00 
c  TempK        0.10089E+05       5   0.46902E-05   0.11669E+02 0.11850E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6884e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.245          19.116       -0.001823      -0.0096744
v  Velocity[Y]             -15.608          14.913         0.16995         0.24971
v  Velocity[Z]             -25.489          12.216         -1.6532        -0.50773
v  ǁVelocityǁ         0.00022528          25.664          7.7513          6.7291
v  Pressure                -524.09          202.59          25.571          28.994
v  k                   9.9331e-011          7.9492         0.18358         0.38449
v  omega                    57.486     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17           335.4          342.36
v  TurbVisc            2.4893e-018       0.0012776     4.5093e-005      0.00016065
v  CourantNb            0.00014682          1.4951         0.79436         0.97561
v  FourierNb             0.0037646               1         0.40433         0.14611
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040572     7.3286e-005      0.00019789

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.26          306.39
v  Yplus               0          2.9246         0.63428         0.49154


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.29869          2.0874          1.1987          1.1217


 INSTANT    0.600000000E-02   TIME STEP NUMBER             600
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925303E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16127E-01 0.46818E+01
   Friction velocity        uk    :  0.16127E-01 0.46778E+01
   Dimensionless distance   yplus :  0.10934E-01 0.29244E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.15667E+03
   Rough dim-less th. sca.  tplus :  0.77459E-02 0.20717E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27784E+00       9   0.87167E-05   0.27151E+01 0.26193E+02 
c  Velocity[X]                                      0.11756E+01 
c  Velocity[Y]                                      0.69282E+00 
c  Velocity[Z]                                      0.84668E+00 
c  Pressure     0.12605E-04      15   0.21822E-03   0.12491E-01 0.84393E+01 
c  k            0.14970E-01      11   0.24639E-04   0.37321E-01 0.41028E+02 
c  omega        0.27922E+07       1   0.68877E-07   0.11069E+08 0.52402E+00 
c  TempK        0.10089E+05       5   0.46779E-05   0.11604E+02 0.11816E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6888e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.245          19.115      -0.0017121      -0.0096083
v  Velocity[Y]             -15.507          14.913         0.17034         0.25024
v  Velocity[Z]             -25.487          12.216         -1.6531         -0.5077
v  ǁVelocityǁ         0.00022162          25.662           7.751          6.7286
v  Pressure                -523.99          202.56           25.55          28.979
v  k                   9.9324e-011          7.9532         0.18384         0.38514
v  omega                    57.486     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17          335.41          342.39
v  TurbVisc            2.4891e-018       0.0012815     4.5157e-005      0.00016091
v  CourantNb            0.00014697           1.495         0.79434         0.97561
v  FourierNb             0.0037648               1         0.40439         0.14626
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.004053     7.3287e-005       0.0001979

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.26          306.39
v  Yplus               0          2.9244         0.63426         0.49151


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.444          2.0873          1.1987          1.1219


 INSTANT    0.601000000E-02   TIME STEP NUMBER             601
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925434E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16114E-01 0.46818E+01
   Friction velocity        uk    :  0.16114E-01 0.46778E+01
   Dimensionless distance   yplus :  0.10926E-01 0.29243E+01
   Friction thermal sca.    tstar :  0.12115E+01 0.15680E+03
   Rough dim-less th. sca.  tplus :  0.77397E-02 0.20716E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27781E+00       9   0.87032E-05   0.27162E+01 0.26187E+02 
c  Velocity[X]                                      0.11740E+01 
c  Velocity[Y]                                      0.69167E+00 
c  Velocity[Z]                                      0.85053E+00 
c  Pressure     0.12413E-04      15   0.21227E-03   0.12304E-01 0.83572E+01 
c  k            0.14996E-01      11   0.24549E-04   0.37326E-01 0.40972E+02 
c  omega        0.27922E+07       1   0.65319E-07   0.40547E+07 0.34812E+00 
c  TempK        0.10089E+05       5   0.46656E-05   0.11540E+02 0.11783E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.689e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.245          19.115      -0.0016013       -0.009544
v  Velocity[Y]             -15.474          14.914         0.17073         0.25077
v  Velocity[Z]             -25.485          12.216          -1.653        -0.50768
v  ǁVelocityǁ         0.00021811          25.661          7.7507          6.7281
v  Pressure                -523.88          202.54           25.53          28.964
v  k                   9.9317e-011          8.2753         0.18409         0.38578
v  omega                    57.486     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17          335.43          342.41
v  TurbVisc            2.4889e-018       0.0012847     4.5221e-005      0.00016116
v  CourantNb            0.00014713           1.495         0.79433         0.97561
v  FourierNb             0.0037649               1         0.40445          0.1464
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040438     7.3288e-005      0.00019791

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.26          306.39
v  Yplus               0          2.9243         0.63423         0.49148


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55917          2.0873          1.1988           1.122


 INSTANT    0.602000000E-02   TIME STEP NUMBER             602
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925453E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16084E-01 0.46817E+01
   Friction velocity        uk    :  0.16084E-01 0.46777E+01
   Dimensionless distance   yplus :  0.10905E-01 0.29242E+01
   Friction thermal sca.    tstar :  0.12115E+01 0.15708E+03
   Rough dim-less th. sca.  tplus :  0.77255E-02 0.20715E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27779E+00       9   0.86334E-05   0.27189E+01 0.26201E+02 
c  Velocity[X]                                      0.11714E+01 
c  Velocity[Y]                                      0.69238E+00 
c  Velocity[Z]                                      0.85519E+00 
c  Pressure     0.11999E-04      15   0.21357E-03   0.11898E-01 0.84301E+01 
c  k            0.15021E-01      11   0.24275E-04   0.37318E-01 0.40935E+02 
c  omega        0.27922E+07       1   0.65335E-07   0.36792E+07 0.34289E+00 
c  TempK        0.10090E+05       5   0.46534E-05   0.11477E+02 0.11751E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6888e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.246          19.114      -0.0014898      -0.0094825
v  Velocity[Y]             -15.497          14.914         0.17112          0.2513
v  Velocity[Z]             -25.484          12.215         -1.6528        -0.50766
v  ǁVelocityǁ          0.0002145          25.659          7.7503          6.7275
v  Pressure                -523.77          202.51          25.509          28.949
v  k                    9.931e-011          8.8035         0.18435         0.38642
v  omega                    57.486     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17          335.44          342.44
v  TurbVisc            2.4887e-018       0.0012874     4.5285e-005      0.00016142
v  CourantNb            0.00014728           1.495         0.79431         0.97561
v  FourierNb             0.0037651               1         0.40451         0.14655
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040267     7.3289e-005      0.00019793

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.26          306.39
v  Yplus               0          2.9242         0.63421         0.49145


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57859          2.0874          1.1988          1.1222


 INSTANT    0.603000000E-02   TIME STEP NUMBER             603
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925360E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16054E-01 0.46817E+01
   Friction velocity        uk    :  0.16054E-01 0.46777E+01
   Dimensionless distance   yplus :  0.10885E-01 0.29241E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.15738E+03
   Rough dim-less th. sca.  tplus :  0.77111E-02 0.20715E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27776E+00       9   0.86129E-05   0.27235E+01 0.26227E+02 
c  Velocity[X]                                      0.11688E+01 
c  Velocity[Y]                                      0.69331E+00 
c  Velocity[Z]                                      0.86145E+00 
c  Pressure     0.12054E-04      15   0.21425E-03   0.11956E-01 0.81746E+01 
c  k            0.15046E-01      11   0.24081E-04   0.37131E-01 0.40757E+02 
c  omega        0.27922E+07       1   0.68086E-07   0.77972E+07 0.45731E+00 
c  TempK        0.10090E+05       5   0.46413E-05   0.11416E+02 0.11719E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6883e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.246          19.114      -0.0013778      -0.0094231
v  Velocity[Y]             -15.589          14.914         0.17151         0.25184
v  Velocity[Z]             -25.482          12.215         -1.6527        -0.50764
v  ǁVelocityǁ         0.00021079          25.658            7.75           6.727
v  Pressure                -523.65           202.5          25.495          28.941
v  k                   9.9303e-011           8.548          0.1846         0.38705
v  omega                    57.486     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17          335.46          342.46
v  TurbVisc            2.4886e-018       0.0012895     4.5348e-005      0.00016167
v  CourantNb            0.00014743          1.4951         0.79429          0.9756
v  FourierNb             0.0037653               1         0.40457         0.14669
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040006      7.329e-005      0.00019794

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.26          306.39
v  Yplus               0          2.9241          0.6342         0.49142


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65556          2.0875          1.1989          1.1223


 INSTANT    0.604000000E-02   TIME STEP NUMBER             604
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925330E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16016E-01 0.46817E+01
   Friction velocity        uk    :  0.16016E-01 0.46777E+01
   Dimensionless distance   yplus :  0.10859E-01 0.29240E+01
   Friction thermal sca.    tstar :  0.12115E+01 0.15775E+03
   Rough dim-less th. sca.  tplus :  0.76929E-02 0.20714E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27774E+00       9   0.86072E-05   0.27310E+01 0.26276E+02 
c  Velocity[X]                                      0.11668E+01 
c  Velocity[Y]                                      0.69653E+00 
c  Velocity[Z]                                      0.86769E+00 
c  Pressure     0.11817E-04      15   0.21500E-03   0.11723E-01 0.82071E+01 
c  k            0.15071E-01      11   0.23967E-04   0.37128E-01 0.40739E+02 
c  omega        0.27922E+07       1   0.70311E-07   0.11980E+08 0.54900E+00 
c  TempK        0.10091E+05       5   0.46293E-05   0.11354E+02 0.11688E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6878e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.247          19.114      -0.0012638      -0.0093669
v  Velocity[Y]             -15.648          14.914         0.17189         0.25237
v  Velocity[Z]             -25.481          12.215         -1.6526        -0.50762
v  ǁVelocityǁ         0.00020521          25.656          7.7497          6.7265
v  Pressure                -523.52          202.48          25.482          28.933
v  k                   9.9296e-011          8.1523         0.18485         0.38768
v  omega                    57.485     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17          335.47          342.49
v  TurbVisc            2.4884e-018        0.001291     4.5411e-005      0.00016192
v  CourantNb            0.00014756          1.4953         0.79427          0.9756
v  FourierNb             0.0037655               1         0.40463         0.14683
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0039664     7.3292e-005      0.00019795

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.26          306.39
v  Yplus               0           2.924         0.63418         0.49139


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73893          2.0877          1.1989          1.1224


 INSTANT    0.605000000E-02   TIME STEP NUMBER             605
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925293E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15971E-01 0.46816E+01
   Friction velocity        uk    :  0.15971E-01 0.46777E+01
   Dimensionless distance   yplus :  0.10828E-01 0.29240E+01
   Friction thermal sca.    tstar :  0.12115E+01 0.15820E+03
   Rough dim-less th. sca.  tplus :  0.76709E-02 0.20714E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27771E+00       9   0.86085E-05   0.27409E+01 0.26341E+02 
c  Velocity[X]                                      0.11659E+01 
c  Velocity[Y]                                      0.70202E+00 
c  Velocity[Z]                                      0.87295E+00 
c  Pressure     0.11876E-04      15   0.21168E-03   0.11783E-01 0.85331E+01 
c  k            0.15096E-01      11   0.23710E-04   0.37131E-01 0.40716E+02 
c  omega        0.27922E+07       1   0.71726E-07   0.13367E+08 0.57844E+00 
c  TempK        0.10091E+05       5   0.46173E-05   0.11293E+02 0.11656E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6879e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.248          19.113      -0.0011507      -0.0093122
v  Velocity[Y]             -15.575          14.914         0.17229          0.2529
v  Velocity[Z]             -25.479          12.214         -1.6525         -0.5076
v  ǁVelocityǁ         0.00019981          25.654          7.7494          6.7259
v  Pressure                 -523.4          202.46          25.469          28.925
v  k                   9.9289e-011          7.9626          0.1851          0.3883
v  omega                    57.485     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17          335.49          342.52
v  TurbVisc            2.4882e-018       0.0012919     4.5474e-005      0.00016216
v  CourantNb            0.00014772          1.4952         0.79425         0.97559
v  FourierNb             0.0037656               1         0.40469         0.14697
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0039248     7.3294e-005      0.00019797

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.27           306.4
v  Yplus               0           2.924         0.63416         0.49136


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66536          2.0877          1.1989          1.1226


 INSTANT    0.606000000E-02   TIME STEP NUMBER             606
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925169E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15955E-01 0.46816E+01
   Friction velocity        uk    :  0.15955E-01 0.46776E+01
   Dimensionless distance   yplus :  0.10818E-01 0.29238E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.15836E+03
   Rough dim-less th. sca.  tplus :  0.76634E-02 0.20712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27769E+00       9   0.85861E-05   0.27460E+01 0.26346E+02 
c  Velocity[X]                                      0.11665E+01 
c  Velocity[Y]                                      0.70261E+00 
c  Velocity[Z]                                      0.87689E+00 
c  Pressure     0.11968E-04      15   0.21596E-03   0.11877E-01 0.82852E+01 
c  k            0.15121E-01      11   0.23570E-04   0.37033E-01 0.40625E+02 
c  omega        0.27922E+07       1   0.69545E-07   0.91812E+07 0.49569E+00 
c  TempK        0.10091E+05       5   0.46055E-05   0.11231E+02 0.11623E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6882e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.249          19.113      -0.0010352      -0.0092603
v  Velocity[Y]             -15.513          14.914         0.17268         0.25344
v  Velocity[Z]             -25.477          12.214         -1.6524        -0.50759
v  ǁVelocityǁ         0.00019421          25.653           7.749          6.7254
v  Pressure                -523.29          202.45          25.456          28.917
v  k                   9.9283e-011          7.9952         0.18535         0.38892
v  omega                    57.485     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17           335.5          342.54
v  TurbVisc             2.488e-018       0.0012924     4.5536e-005      0.00016241
v  CourantNb            0.00014788          1.4952         0.79423         0.97559
v  FourierNb             0.0037658               1         0.40474         0.14711
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0038779     7.3297e-005      0.00019799

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.27           306.4
v  Yplus               0          2.9238         0.63414         0.49133


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6015          2.0876           1.199          1.1227


 INSTANT    0.607000000E-02   TIME STEP NUMBER             607
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925409E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15940E-01 0.46816E+01
   Friction velocity        uk    :  0.15940E-01 0.46776E+01
   Dimensionless distance   yplus :  0.10808E-01 0.29237E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.15851E+03
   Rough dim-less th. sca.  tplus :  0.76561E-02 0.20712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27767E+00       9   0.86042E-05   0.27483E+01 0.26323E+02 
c  Velocity[X]                                      0.11650E+01 
c  Velocity[Y]                                      0.70161E+00 
c  Velocity[Z]                                      0.88170E+00 
c  Pressure     0.12008E-04      15   0.21145E-03   0.11918E-01 0.85846E+01 
c  k            0.15146E-01      11   0.23321E-04   0.36987E-01 0.40592E+02 
c  omega        0.27922E+07       1   0.68986E-07   0.79392E+07 0.47214E+00 
c  TempK        0.10092E+05       5   0.45936E-05   0.11170E+02 0.11592E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6883e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.249          19.112     -0.00091951      -0.0092115
v  Velocity[Y]             -15.498          14.915         0.17308         0.25398
v  Velocity[Z]             -25.476          12.214         -1.6523        -0.50757
v  ǁVelocityǁ         0.00018917          25.651          7.7487          6.7249
v  Pressure                -523.18          202.42          25.434          28.901
v  k                   9.9276e-011          8.3425          0.1856         0.38954
v  omega                    57.485     2.7322e+008     1.2912e+006           76901
v  TempK                     298.5          363.17          335.52          342.57
v  TurbVisc            2.4879e-018       0.0012923     4.5598e-005      0.00016265
v  CourantNb            0.00014804          1.4951         0.79421         0.97559
v  FourierNb              0.003766               1          0.4048         0.14725
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0038271       7.33e-005        0.000198

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.27           306.4
v  Yplus               0          2.9237         0.63411          0.4913


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55749          2.0876           1.199          1.1228


 INSTANT    0.608000000E-02   TIME STEP NUMBER             608
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925501E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15911E-01 0.46816E+01
   Friction velocity        uk    :  0.15911E-01 0.46776E+01
   Dimensionless distance   yplus :  0.10788E-01 0.29236E+01
   Friction thermal sca.    tstar :  0.12115E+01 0.15880E+03
   Rough dim-less th. sca.  tplus :  0.76423E-02 0.20711E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27764E+00       9   0.86256E-05   0.27548E+01 0.26340E+02 
c  Velocity[X]                                      0.11651E+01 
c  Velocity[Y]                                      0.70322E+00 
c  Velocity[Z]                                      0.88649E+00 
c  Pressure     0.12039E-04      15   0.21705E-03   0.11951E-01 0.84303E+01 
c  k            0.15170E-01      11   0.23138E-04   0.36877E-01 0.40497E+02 
c  omega        0.27922E+07       1   0.68167E-07   0.61539E+07 0.42842E+00 
c  TempK        0.10092E+05       5   0.45819E-05   0.11110E+02 0.11560E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6881e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.25          19.112     -0.00080216      -0.0091658
v  Velocity[Y]             -15.531          14.915         0.17348         0.25452
v  Velocity[Z]             -25.474          12.213         -1.6522        -0.50755
v  ǁVelocityǁ         0.00018416          25.649          7.7484          6.7244
v  Pressure                -523.06           202.4          25.415          28.887
v  k                    9.927e-011          8.1923         0.18585         0.39015
v  omega                    57.485     2.7322e+008     1.2912e+006           76900
v  TempK                     298.5          363.17          335.53           342.6
v  TurbVisc            2.4877e-018       0.0012918      4.566e-005      0.00016289
v  CourantNb            0.00014817          1.4952         0.79419         0.97558
v  FourierNb             0.0037661               1         0.40486         0.14739
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0037734     7.3303e-005      0.00019802

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.27           306.4
v  Yplus               0          2.9236         0.63409         0.49127


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59362          2.0877          1.1991           1.123


 INSTANT    0.609000000E-02   TIME STEP NUMBER             609
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925521E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15879E-01 0.46815E+01
   Friction velocity        uk    :  0.15879E-01 0.46776E+01
   Dimensionless distance   yplus :  0.10766E-01 0.29235E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.15912E+03
   Rough dim-less th. sca.  tplus :  0.76268E-02 0.20710E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27762E+00       9   0.86460E-05   0.27664E+01 0.26401E+02 
c  Velocity[X]                                      0.11657E+01 
c  Velocity[Y]                                      0.70681E+00 
c  Velocity[Z]                                      0.89385E+00 
c  Pressure     0.12174E-04      15   0.21484E-03   0.12087E-01 0.85610E+01 
c  k            0.15195E-01      11   0.23043E-04   0.36887E-01 0.40479E+02 
c  omega        0.27922E+07       1   0.70628E-07   0.98820E+07 0.51436E+00 
c  TempK        0.10093E+05       5   0.45702E-05   0.11053E+02 0.11530E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6876e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.251          19.111     -0.00068236       -0.009123
v  Velocity[Y]             -15.673          14.915         0.17387         0.25507
v  Velocity[Z]             -25.472          12.212         -1.6521        -0.50753
v  ǁVelocityǁ         0.00017964          25.648           7.748          6.7238
v  Pressure                -522.93          202.38          25.398          28.875
v  k                   9.9263e-011          7.9336         0.18609         0.39076
v  omega                    57.485     2.7322e+008     1.2912e+006           76900
v  TempK                     298.5          363.17          335.55          342.62
v  TurbVisc            2.4876e-018       0.0012908     4.5721e-005      0.00016313
v  CourantNb             0.0001483          1.4953         0.79418         0.97558
v  FourierNb             0.0037663               1         0.40491         0.14753
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0037167     7.3306e-005      0.00019804

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.27           306.4
v  Yplus               0          2.9235         0.63407         0.49124


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62999          2.0879          1.1991          1.1231


 INSTANT    0.610000000E-02   TIME STEP NUMBER             610
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925388E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15820E-01 0.46815E+01
   Friction velocity        uk    :  0.15820E-01 0.46775E+01
   Dimensionless distance   yplus :  0.10727E-01 0.29234E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.16062E+03
   Rough dim-less th. sca.  tplus :  0.75987E-02 0.20710E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27760E+00       9   0.86725E-05   0.27793E+01 0.26473E+02 
c  Velocity[X]                                      0.11673E+01 
c  Velocity[Y]                                      0.71380E+00 
c  Velocity[Z]                                      0.89820E+00 
c  Pressure     0.12348E-04      15   0.21725E-03   0.12261E-01 0.82624E+01 
c  k            0.15219E-01      11   0.22917E-04   0.36914E-01 0.40454E+02 
c  omega        0.27922E+07       1   0.70727E-07   0.10268E+08 0.52817E+00 
c  TempK        0.10093E+05       5   0.45586E-05   0.10996E+02 0.11499E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6878e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.252          19.111     -0.00056088      -0.0090841
v  Velocity[Y]             -15.597          14.915         0.17427         0.25561
v  Velocity[Z]             -25.471          12.212          -1.652        -0.50751
v  ǁVelocityǁ         0.00017457          25.646          7.7477          6.7233
v  Pressure                -522.81          202.36          25.383          28.866
v  k                   9.9257e-011          7.9159         0.18634         0.39136
v  omega                    57.485     2.7322e+008     1.2912e+006           76900
v  TempK                     298.5          363.17          335.56          342.65
v  TurbVisc            2.4874e-018       0.0012893     4.5782e-005      0.00016336
v  CourantNb            0.00014841          1.4953         0.79416         0.97558
v  FourierNb             0.0037665               1         0.40497         0.14767
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0036581     7.3309e-005      0.00019805

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.27           306.4
v  Yplus               0          2.9234         0.63405         0.49121


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61642          2.0878          1.1991          1.1232


 INSTANT    0.611000000E-02   TIME STEP NUMBER             611
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925402E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15670E-01 0.46815E+01
   Friction velocity        uk    :  0.15670E-01 0.46775E+01
   Dimensionless distance   yplus :  0.10624E-01 0.29233E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.16305E+03
   Rough dim-less th. sca.  tplus :  0.75264E-02 0.20709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27757E+00       9   0.86984E-05   0.27855E+01 0.26465E+02 
c  Velocity[X]                                      0.11691E+01 
c  Velocity[Y]                                      0.71308E+00 
c  Velocity[Z]                                      0.90322E+00 
c  Pressure     0.12928E-04      15   0.21502E-03   0.12839E-01 0.84893E+01 
c  k            0.15243E-01      11   0.22849E-04   0.36919E-01 0.40406E+02 
c  omega        0.27922E+07       1   0.70645E-07   0.10311E+08 0.52421E+00 
c  TempK        0.10093E+05       5   0.45471E-05   0.10941E+02 0.11470E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6883e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.252           19.11     -0.00043674      -0.0090469
v  Velocity[Y]             -15.535          14.916         0.17467         0.25615
v  Velocity[Z]             -25.469          12.211          -1.652         -0.5075
v  ǁVelocityǁ          0.0001698          25.645          7.7474          6.7228
v  Pressure                 -522.7          202.34          25.364          28.852
v  k                   9.9251e-011          7.8931         0.18659         0.39196
v  omega                    57.485     2.7322e+008     1.2912e+006           76900
v  TempK                     298.5          363.17          335.58          342.67
v  TurbVisc            2.4872e-018       0.0012872     4.5842e-005       0.0001636
v  CourantNb            0.00014854          1.4952         0.79414         0.97558
v  FourierNb             0.0037667               1         0.40503          0.1478
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.003599     7.3312e-005      0.00019807

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.27           306.4
v  Yplus               0          2.9233         0.63403         0.49119


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72518          2.0878          1.1992          1.1234


 INSTANT    0.612000000E-02   TIME STEP NUMBER             612
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925370E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15443E-01 0.46815E+01
   Friction velocity        uk    :  0.15443E-01 0.46775E+01
   Dimensionless distance   yplus :  0.10470E-01 0.29232E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.16545E+03
   Rough dim-less th. sca.  tplus :  0.74173E-02 0.20708E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27755E+00       9   0.87490E-05   0.27987E+01 0.26530E+02 
c  Velocity[X]                                      0.11725E+01 
c  Velocity[Y]                                      0.71689E+00 
c  Velocity[Z]                                      0.90931E+00 
c  Pressure     0.12762E-04      15   0.22093E-03   0.12675E-01 0.83905E+01 
c  k            0.15267E-01      11   0.22852E-04   0.37060E-01 0.40437E+02 
c  omega        0.27922E+07       1   0.70439E-07   0.91971E+07 0.49623E+00 
c  TempK        0.10094E+05       5   0.45356E-05   0.10889E+02 0.11442E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6885e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253           19.11     -0.00031139      -0.0090129
v  Velocity[Y]             -15.503          14.916         0.17507          0.2567
v  Velocity[Z]             -25.468          12.211         -1.6519        -0.50749
v  ǁVelocityǁ         0.00016451          25.643           7.747          6.7222
v  Pressure                -522.58          202.33          25.351          28.845
v  k                   9.9245e-011          8.1363         0.18683         0.39255
v  omega                    57.485     2.7322e+008     1.2912e+006           76900
v  TempK                    298.51          363.17          335.59           342.7
v  TurbVisc            2.4871e-018       0.0012847     4.5902e-005      0.00016383
v  CourantNb            0.00014867          1.4951         0.79413         0.97557
v  FourierNb             0.0037668               1         0.40509         0.14793
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0035399     7.3315e-005      0.00019809

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.28           306.4
v  Yplus               0          2.9232         0.63401         0.49115


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.796          2.0878          1.1992          1.1235


 INSTANT    0.613000000E-02   TIME STEP NUMBER             613
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925282E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15187E-01 0.46814E+01
   Friction velocity        uk    :  0.15187E-01 0.46775E+01
   Dimensionless distance   yplus :  0.10297E-01 0.29231E+01
   Friction thermal sca.    tstar :  0.12119E+01 0.16823E+03
   Rough dim-less th. sca.  tplus :  0.72946E-02 0.20708E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27753E+00       9   0.87881E-05   0.28129E+01 0.26613E+02 
c  Velocity[X]                                      0.11760E+01 
c  Velocity[Y]                                      0.72309E+00 
c  Velocity[Z]                                      0.91379E+00 
c  Pressure     0.12439E-04      15   0.22274E-03   0.12356E-01 0.83895E+01 
c  k            0.15291E-01      11   0.22941E-04   0.37160E-01 0.40421E+02 
c  omega        0.27922E+07       1   0.69949E-07   0.87262E+07 0.48807E+00 
c  TempK        0.10094E+05       5   0.45242E-05   0.10837E+02 0.11413E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6883e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.109     -0.00018376      -0.0089809
v  Velocity[Y]              -15.52          14.916         0.17547         0.25726
v  Velocity[Z]             -25.466           12.21         -1.6518        -0.50748
v  ǁVelocityǁ          0.0001601          25.641          7.7467          6.7217
v  Pressure                -522.47          202.31          25.334          28.834
v  k                   9.9239e-011          8.0215         0.18707         0.39314
v  omega                    57.485     2.7322e+008     1.2912e+006           76900
v  TempK                    298.51          363.17          335.61          342.72
v  TurbVisc            2.4869e-018       0.0012817     4.5962e-005      0.00016406
v  CourantNb            0.00014882          1.4951         0.79411         0.97557
v  FourierNb              0.003767               1         0.40514         0.14807
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0036185     7.3318e-005       0.0001981

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.28           306.4
v  Yplus               0          2.9231         0.63399         0.49112


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7551          2.0878          1.1993          1.1236


 INSTANT    0.614000000E-02   TIME STEP NUMBER             614
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925355E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14971E-01 0.46814E+01
   Friction velocity        uk    :  0.14970E-01 0.46774E+01
   Dimensionless distance   yplus :  0.10150E-01 0.29230E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.17067E+03
   Rough dim-less th. sca.  tplus :  0.71905E-02 0.20707E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27751E+00      10   0.75570E-05   0.28255E+01 0.26649E+02 
c  Velocity[X]                                      0.11800E+01 
c  Velocity[Y]                                      0.72504E+00 
c  Velocity[Z]                                      0.92047E+00 
c  Pressure     0.12362E-04      15   0.22999E-03   0.12281E-01 0.84456E+01 
c  k            0.15315E-01      11   0.23044E-04   0.37313E-01 0.40445E+02 
c  omega        0.27922E+07       1   0.71146E-07   0.10818E+08 0.53144E+00 
c  TempK        0.10095E+05       5   0.45129E-05   0.10786E+02 0.11386E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6878e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.254          19.109    -5.5502e-005      -0.0089523
v  Velocity[Y]             -15.584          14.917         0.17588         0.25781
v  Velocity[Z]             -25.464          12.209         -1.6517        -0.50746
v  ǁVelocityǁ         0.00015567           25.64          7.7464          6.7212
v  Pressure                -522.35          202.28          25.315           28.82
v  k                   9.9232e-011          7.8418         0.18732         0.39373
v  omega                    57.485     2.7322e+008     1.2912e+006           76900
v  TempK                    298.51          363.17          335.62          342.75
v  TurbVisc            2.4868e-018       0.0012781     4.6022e-005      0.00016429
v  CourantNb            0.00014893          1.4953         0.79409         0.97557
v  FourierNb             0.0037672               1          0.4052          0.1482
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0039804      7.332e-005      0.00019812

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.28          306.41
v  Yplus               0           2.923         0.63397         0.49109


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.79648           2.088          1.1993          1.1238


 INSTANT    0.615000000E-02   TIME STEP NUMBER             615
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925409E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14749E-01 0.46814E+01
   Friction velocity        uk    :  0.14749E-01 0.46774E+01
   Dimensionless distance   yplus :  0.10000E-01 0.29229E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.17323E+03
   Rough dim-less th. sca.  tplus :  0.70842E-02 0.20706E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27748E+00      10   0.75903E-05   0.28389E+01 0.26721E+02 
c  Velocity[X]                                      0.11830E+01 
c  Velocity[Y]                                      0.72884E+00 
c  Velocity[Z]                                      0.92712E+00 
c  Pressure     0.12088E-04      15   0.22298E-03   0.12009E-01 0.82943E+01 
c  k            0.15339E-01      11   0.23183E-04   0.37530E-01 0.40507E+02 
c  omega        0.27922E+07       1   0.70758E-07   0.94454E+07 0.49823E+00 
c  TempK        0.10095E+05       5   0.45017E-05   0.10739E+02 0.11360E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6871e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.254          19.108     7.6751e-005      -0.0089252
v  Velocity[Y]             -15.646          14.917         0.17628         0.25837
v  Velocity[Z]             -25.463          12.209         -1.6517        -0.50745
v  ǁVelocityǁ         0.00015125          25.638           7.746          6.7206
v  Pressure                -522.23          202.27          25.302          28.812
v  k                   9.9226e-011          7.7484         0.18756         0.39431
v  omega                    57.485     2.7322e+008     1.2912e+006           76900
v  TempK                    298.51          363.17          335.63          342.77
v  TurbVisc            2.4866e-018       0.0012741     4.6082e-005      0.00016452
v  CourantNb            0.00014904          1.4954         0.79408         0.97557
v  FourierNb             0.0037674               1         0.40525         0.14833
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0043784     7.3324e-005      0.00019814

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.28          306.41
v  Yplus               0          2.9229         0.63394         0.49106


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67925          2.0881          1.1993          1.1239


 INSTANT    0.616000000E-02   TIME STEP NUMBER             616
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925449E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14525E-01 0.46814E+01
   Friction velocity        uk    :  0.14525E-01 0.46774E+01
   Dimensionless distance   yplus :  0.98483E-02 0.29228E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.17590E+03
   Rough dim-less th. sca.  tplus :  0.69766E-02 0.20705E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27746E+00      10   0.76284E-05   0.28563E+01 0.26815E+02 
c  Velocity[X]                                      0.11881E+01 
c  Velocity[Y]                                      0.73594E+00 
c  Velocity[Z]                                      0.93223E+00 
c  Pressure     0.12418E-04      15   0.23003E-03   0.12338E-01 0.83047E+01 
c  k            0.15362E-01      11   0.23334E-04   0.37762E-01 0.40571E+02 
c  omega        0.27922E+07       1   0.69850E-07   0.87337E+07 0.48661E+00 
c  TempK        0.10095E+05       5   0.44906E-05   0.10687E+02 0.11332E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6872e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255          19.108      0.00021089      -0.0089013
v  Velocity[Y]             -15.603          14.917         0.17667         0.25893
v  Velocity[Z]             -25.461          12.208         -1.6516        -0.50744
v  ǁVelocityǁ         0.00014612          25.637          7.7457          6.7201
v  Pressure                -522.11          202.25          25.287          28.803
v  k                    9.922e-011          7.6977          0.1878         0.39489
v  omega                    57.485     2.7322e+008     1.2912e+006           76900
v  TempK                    298.51          363.17          335.65           342.8
v  TurbVisc            2.4865e-018       0.0012696     4.6142e-005      0.00016474
v  CourantNb            0.00014916          1.4954         0.79406         0.97557
v  FourierNb             0.0037675               1         0.40531         0.14846
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0045822     7.3326e-005      0.00019815

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.28          306.41
v  Yplus               0          2.9228         0.63392         0.49103


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68665          2.0882          1.1994           1.124


 INSTANT    0.617000000E-02   TIME STEP NUMBER             617
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925399E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14261E-01 0.46814E+01
   Friction velocity        uk    :  0.14261E-01 0.46774E+01
   Dimensionless distance   yplus :  0.96691E-02 0.29227E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.17916E+03
   Rough dim-less th. sca.  tplus :  0.68497E-02 0.20705E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27744E+00      10   0.76262E-05   0.28639E+01 0.26830E+02 
c  Velocity[X]                                      0.11908E+01 
c  Velocity[Y]                                      0.73565E+00 
c  Velocity[Z]                                      0.93744E+00 
c  Pressure     0.12007E-04      16   0.22180E-03   0.11930E-01 0.85036E+01 
c  k            0.15386E-01      11   0.23579E-04   0.37931E-01 0.40593E+02 
c  omega        0.27922E+07       1   0.69232E-07   0.72889E+07 0.45104E+00 
c  TempK        0.10096E+05       5   0.44794E-05   0.10637E+02 0.11306E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6875e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255          19.107       0.0003476      -0.0088802
v  Velocity[Y]             -15.502          14.918         0.17707         0.25949
v  Velocity[Z]              -25.46          12.207         -1.6515        -0.50743
v  ǁVelocityǁ         0.00014113          25.635          7.7453          6.7196
v  Pressure                   -522          202.23          25.268           28.79
v  k                   9.9215e-011          7.6408         0.18804         0.39546
v  omega                    57.485     2.7322e+008     1.2912e+006           76900
v  TempK                    298.51          363.17          335.66          342.82
v  TurbVisc            2.4863e-018       0.0012646     4.6201e-005      0.00016497
v  CourantNb            0.00014932          1.4953         0.79404         0.97556
v  FourierNb             0.0037677               1         0.40536         0.14859
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0045406      7.333e-005      0.00019817

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.28          306.41
v  Yplus               0          2.9227          0.6339           0.491


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.663          2.0881          1.1994          1.1242


 INSTANT    0.618000000E-02   TIME STEP NUMBER             618
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925347E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13999E-01 0.46813E+01
   Friction velocity        uk    :  0.13999E-01 0.46774E+01
   Dimensionless distance   yplus :  0.94916E-02 0.29227E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.18251E+03
   Rough dim-less th. sca.  tplus :  0.67239E-02 0.20704E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27742E+00      10   0.76468E-05   0.28763E+01 0.26876E+02 
c  Velocity[X]                                      0.11954E+01 
c  Velocity[Y]                                      0.73797E+00 
c  Velocity[Z]                                      0.94297E+00 
c  Pressure     0.12195E-04      15   0.22738E-03   0.12116E-01 0.82642E+01 
c  k            0.15409E-01      11   0.23840E-04   0.38263E-01 0.40706E+02 
c  omega        0.27922E+07       1   0.68765E-07   0.58478E+07 0.41243E+00 
c  TempK        0.10096E+05       5   0.44683E-05   0.10587E+02 0.11280E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6877e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255          19.107      0.00048568      -0.0088629
v  Velocity[Y]             -15.466          14.918         0.17747         0.26006
v  Velocity[Z]             -25.459          12.207         -1.6514        -0.50742
v  ǁVelocityǁ         0.00013652          25.634           7.745           6.719
v  Pressure                -521.89          202.21          25.254          28.782
v  k                   9.9209e-011          7.7357         0.18827         0.39603
v  omega                    57.485     2.7322e+008     1.2912e+006           76900
v  TempK                    298.51          363.17          335.68          342.85
v  TurbVisc            2.4862e-018       0.0012628      4.626e-005      0.00016519
v  CourantNb            0.00014947          1.4953         0.79402         0.97556
v  FourierNb             0.0037679               1         0.40542         0.14872
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0044911     7.3333e-005      0.00019819

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.29          306.41
v  Yplus               0          2.9227         0.63388         0.49097


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48467          2.0881          1.1994          1.1243


 INSTANT    0.619000000E-02   TIME STEP NUMBER             619
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925235E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13752E-01 0.46813E+01
   Friction velocity        uk    :  0.13752E-01 0.46773E+01
   Dimensionless distance   yplus :  0.93242E-02 0.29226E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.18579E+03
   Rough dim-less th. sca.  tplus :  0.66054E-02 0.20704E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27740E+00      10   0.76783E-05   0.28910E+01 0.26966E+02 
c  Velocity[X]                                      0.11999E+01 
c  Velocity[Y]                                      0.74228E+00 
c  Velocity[Z]                                      0.94881E+00 
c  Pressure     0.12036E-04      15   0.22770E-03   0.11959E-01 0.83478E+01 
c  k            0.15432E-01      11   0.24119E-04   0.38615E-01 0.40839E+02 
c  omega        0.27922E+07       1   0.70897E-07   0.88573E+07 0.48486E+00 
c  TempK        0.10097E+05       5   0.44573E-05   0.10539E+02 0.11256E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6875e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255          19.106      0.00062562      -0.0088476
v  Velocity[Y]             -15.487          14.919         0.17788         0.26062
v  Velocity[Z]             -25.457          12.206         -1.6514        -0.50741
v  ǁVelocityǁ         0.00013158          25.633          7.7447          6.7185
v  Pressure                -521.77           202.2          25.246          28.779
v  k                   9.9203e-011          8.2114         0.18851         0.39659
v  omega                    57.484     2.7322e+008     1.2912e+006           76900
v  TempK                    298.51          363.17          335.69          342.87
v  TurbVisc             2.486e-018       0.0012678     4.6318e-005      0.00016541
v  CourantNb             0.0001496          1.4953         0.79401         0.97556
v  FourierNb             0.0037681               1         0.40548         0.14885
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0044047     7.3336e-005      0.00019821

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.29          306.41
v  Yplus               0          2.9226         0.63385         0.49093


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69587          2.0882          1.1995          1.1244


 INSTANT    0.620000000E-02   TIME STEP NUMBER             620
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925158E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13482E-01 0.46813E+01
   Friction velocity        uk    :  0.13482E-01 0.46773E+01
   Dimensionless distance   yplus :  0.91413E-02 0.29224E+01
   Friction thermal sca.    tstar :  0.12119E+01 0.18951E+03
   Rough dim-less th. sca.  tplus :  0.64758E-02 0.20703E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27738E+00      10   0.77124E-05   0.29104E+01 0.27079E+02 
c  Velocity[X]                                      0.12059E+01 
c  Velocity[Y]                                      0.74892E+00 
c  Velocity[Z]                                      0.95560E+00 
c  Pressure     0.12257E-04      15   0.22643E-03   0.12179E-01 0.82250E+01 
c  k            0.15456E-01      11   0.24368E-04   0.38871E-01 0.40884E+02 
c  omega        0.27922E+07       1   0.73036E-07   0.12768E+08 0.56697E+00 
c  TempK        0.10097E+05       5   0.44464E-05   0.10492E+02 0.11230E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6869e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255          19.105      0.00076869      -0.0088357
v  Velocity[Y]             -15.578           14.92         0.17828         0.26119
v  Velocity[Z]             -25.455          12.205         -1.6513         -0.5074
v  ǁVelocityǁ         0.00012726          25.631          7.7443          6.7179
v  Pressure                -521.65          202.19          25.236          28.774
v  k                   9.9197e-011          7.9737         0.18875         0.39716
v  omega                    57.484     2.7322e+008     1.2912e+006           76900
v  TempK                    298.51          363.17          335.71           342.9
v  TurbVisc            2.4859e-018       0.0012727     4.6377e-005      0.00016563
v  CourantNb            0.00014976          1.4955         0.79399         0.97556
v  FourierNb             0.0037682               1         0.40553         0.14897
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0042871     7.3339e-005      0.00019823

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.29          306.41
v  Yplus               0          2.9224         0.63383          0.4909


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77801          2.0883          1.1995          1.1245


 INSTANT    0.621000000E-02   TIME STEP NUMBER             621
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925380E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13242E-01 0.46813E+01
   Friction velocity        uk    :  0.13242E-01 0.46773E+01
   Dimensionless distance   yplus :  0.89780E-02 0.29223E+01
   Friction thermal sca.    tstar :  0.12119E+01 0.19296E+03
   Rough dim-less th. sca.  tplus :  0.63601E-02 0.20702E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27736E+00      10   0.77468E-05   0.29227E+01 0.27134E+02 
c  Velocity[X]                                      0.12099E+01 
c  Velocity[Y]                                      0.75221E+00 
c  Velocity[Z]                                      0.96056E+00 
c  Pressure     0.12119E-04      15   0.22744E-03   0.12043E-01 0.85985E+01 
c  k            0.15478E-01      11   0.24680E-04   0.39269E-01 0.41029E+02 
c  omega        0.27922E+07       1   0.73383E-07   0.13975E+08 0.58937E+00 
c  TempK        0.10097E+05       5   0.44355E-05   0.10446E+02 0.11205E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6862e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255          19.105      0.00091754      -0.0088261
v  Velocity[Y]             -15.637           14.92         0.17867         0.26177
v  Velocity[Z]             -25.454          12.204         -1.6513        -0.50739
v  ǁVelocityǁ         0.00012206          25.629           7.744          6.7174
v  Pressure                -521.53          202.17          25.219          28.762
v  k                   9.9191e-011          7.6011         0.18898         0.39771
v  omega                    57.484     2.7322e+008     1.2912e+006           76900
v  TempK                    298.51          363.17          335.72          342.92
v  TurbVisc            2.4857e-018       0.0012776     4.6435e-005      0.00016584
v  CourantNb            0.00014987          1.4956         0.79397         0.97556
v  FourierNb             0.0037684               1         0.40559          0.1491
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0041485     7.3343e-005      0.00019825

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.29          306.41
v  Yplus               0          2.9223         0.63381         0.49087


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69392          2.0885          1.1996          1.1247


 INSTANT    0.622000000E-02   TIME STEP NUMBER             622
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925414E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12946E-01 0.46812E+01
   Friction velocity        uk    :  0.12946E-01 0.46773E+01
   Dimensionless distance   yplus :  0.87776E-02 0.29223E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.19736E+03
   Rough dim-less th. sca.  tplus :  0.62181E-02 0.20702E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27734E+00      10   0.77902E-05   0.29383E+01 0.27216E+02 
c  Velocity[X]                                      0.12146E+01 
c  Velocity[Y]                                      0.75861E+00 
c  Velocity[Z]                                      0.96511E+00 
c  Pressure     0.12326E-04      15   0.22995E-03   0.12249E-01 0.84897E+01 
c  k            0.15501E-01      11   0.24962E-04   0.39641E-01 0.41140E+02 
c  omega        0.27922E+07       1   0.70568E-07   0.83382E+07 0.47256E+00 
c  TempK        0.10098E+05       5   0.44245E-05   0.10402E+02 0.11181E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6862e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255          19.104       0.0010658      -0.0088192
v  Velocity[Y]             -15.565          14.921         0.17907         0.26234
v  Velocity[Z]             -25.452          12.204         -1.6512        -0.50739
v  ǁVelocityǁ         0.00011742          25.628          7.7436          6.7169
v  Pressure                -521.42          202.15          25.203          28.752
v  k                   9.9186e-011          7.4413         0.18922         0.39826
v  omega                    57.484     2.7322e+008     1.2912e+006           76899
v  TempK                    298.52          363.17          335.73          342.95
v  TurbVisc            2.4856e-018       0.0012825     4.6493e-005      0.00016606
v  CourantNb            0.00015004          1.4956         0.79395         0.97555
v  FourierNb             0.0037686               1         0.40564         0.14923
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0038531     7.3346e-005      0.00019826

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.29          306.41
v  Yplus               0          2.9223         0.63378         0.49084


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6673          2.0885          1.1996          1.1248


 INSTANT    0.623000000E-02   TIME STEP NUMBER             623
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925335E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12676E-01 0.46812E+01
   Friction velocity        uk    :  0.12676E-01 0.46772E+01
   Dimensionless distance   yplus :  0.85944E-02 0.29222E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.20157E+03
   Rough dim-less th. sca.  tplus :  0.60883E-02 0.20701E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27732E+00      10   0.78293E-05   0.29481E+01 0.27240E+02 
c  Velocity[X]                                      0.12199E+01 
c  Velocity[Y]                                      0.75853E+00 
c  Velocity[Z]                                      0.96965E+00 
c  Pressure     0.12439E-04      15   0.22956E-03   0.12363E-01 0.84652E+01 
c  k            0.15524E-01      11   0.25302E-04   0.39942E-01 0.41213E+02 
c  omega        0.27922E+07       1   0.68549E-07   0.41633E+07 0.36208E+00 
c  TempK        0.10098E+05       5   0.44138E-05   0.10360E+02 0.11158E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6864e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.254          19.104       0.0012156      -0.0088146
v  Velocity[Y]             -15.504          14.921         0.17947         0.26292
v  Velocity[Z]             -25.451          12.203         -1.6512        -0.50738
v  ǁVelocityǁ         0.00011245          25.627          7.7433          6.7163
v  Pressure                -521.31          202.13          25.188          28.743
v  k                    9.918e-011          7.5207         0.18945         0.39881
v  omega                    57.484     2.7322e+008     1.2912e+006           76899
v  TempK                    298.52          363.17          335.75          342.97
v  TurbVisc            2.4855e-018       0.0012871     4.6551e-005      0.00016627
v  CourantNb            0.00015018          1.4956         0.79394         0.97555
v  FourierNb             0.0037688               1          0.4057         0.14935
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0033874      7.335e-005      0.00019828

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.29          306.41
v  Yplus               0          2.9222         0.63375         0.49081


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58271          2.0885          1.1996          1.1249


 INSTANT    0.624000000E-02   TIME STEP NUMBER             624
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925276E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12380E-01 0.46812E+01
   Friction velocity        uk    :  0.12380E-01 0.46772E+01
   Dimensionless distance   yplus :  0.83936E-02 0.29221E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.20639E+03
   Rough dim-less th. sca.  tplus :  0.59461E-02 0.20700E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27730E+00      10   0.78782E-05   0.29649E+01 0.27318E+02 
c  Velocity[X]                                      0.12266E+01 
c  Velocity[Y]                                      0.76297E+00 
c  Velocity[Z]                                      0.97539E+00 
c  Pressure     0.12666E-04      15   0.23067E-03   0.12590E-01 0.84049E+01 
c  k            0.15547E-01      11   0.25605E-04   0.40326E-01 0.41340E+02 
c  omega        0.27922E+07       1   0.68501E-07   0.38832E+07 0.35568E+00 
c  TempK        0.10099E+05       5   0.44032E-05   0.10318E+02 0.11135E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6864e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.254          19.103        0.001366      -0.0088107
v  Velocity[Y]             -15.489          14.922         0.17987          0.2635
v  Velocity[Z]              -25.45          12.202         -1.6511        -0.50737
v  ǁVelocityǁ         0.00010729          25.626          7.7429          6.7158
v  Pressure                 -521.2          202.12          25.175          28.735
v  k                   9.9175e-011          7.7325         0.18969         0.39936
v  omega                    57.484     2.7322e+008     1.2912e+006           76899
v  TempK                    298.52          363.17          335.76             343
v  TurbVisc            2.4853e-018       0.0012914     4.6608e-005      0.00016649
v  CourantNb            0.00015034          1.4956         0.79392         0.97555
v  FourierNb              0.003769               1         0.40575         0.14948
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0032833     7.3353e-005       0.0001983

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.29          306.42
v  Yplus               0          2.9221         0.63373         0.49078


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73138          2.0885          1.1997           1.125


 INSTANT    0.625000000E-02   TIME STEP NUMBER             625
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925260E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12064E-01 0.46812E+01
   Friction velocity        uk    :  0.12063E-01 0.46772E+01
   Dimensionless distance   yplus :  0.81793E-02 0.29220E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.21180E+03
   Rough dim-less th. sca.  tplus :  0.57942E-02 0.20700E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27728E+00      10   0.79086E-05   0.29814E+01 0.27399E+02 
c  Velocity[X]                                      0.12321E+01 
c  Velocity[Y]                                      0.76763E+00 
c  Velocity[Z]                                      0.98164E+00 
c  Pressure     0.12715E-04      15   0.23151E-03   0.12640E-01 0.82335E+01 
c  k            0.15569E-01      11   0.25965E-04   0.40665E-01 0.41424E+02 
c  omega        0.27922E+07       1   0.70845E-07   0.77961E+07 0.45898E+00 
c  TempK        0.10099E+05       5   0.43926E-05   0.10276E+02 0.11113E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.686e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.102        0.001516      -0.0088084
v  Velocity[Y]             -15.521          14.923         0.18026         0.26408
v  Velocity[Z]             -25.449          12.201         -1.6511        -0.50737
v  ǁVelocityǁ          0.0001022          25.624          7.7426          6.7153
v  Pressure                -521.08           202.1          25.165          28.731
v  k                   9.9169e-011          7.6675         0.18992          0.3999
v  omega                    57.484     2.7322e+008     1.2912e+006           76899
v  TempK                    298.52          363.17          335.78          343.02
v  TurbVisc            2.4852e-018       0.0012955     4.6666e-005       0.0001667
v  CourantNb            0.00015052          1.4957          0.7939         0.97555
v  FourierNb             0.0037691               1         0.40581          0.1496
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0031892     7.3357e-005      0.00019832

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.3          306.42
v  Yplus               0           2.922         0.63371         0.49075


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48858          2.0886          1.1997          1.1251


 INSTANT    0.626000000E-02   TIME STEP NUMBER             626
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925229E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11743E-01 0.46811E+01
   Friction velocity        uk    :  0.11743E-01 0.46772E+01
   Dimensionless distance   yplus :  0.79621E-02 0.29220E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.21758E+03
   Rough dim-less th. sca.  tplus :  0.56404E-02 0.20699E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27726E+00      10   0.79510E-05   0.30039E+01 0.27537E+02 
c  Velocity[X]                                      0.12375E+01 
c  Velocity[Y]                                      0.77453E+00 
c  Velocity[Z]                                      0.99188E+00 
c  Pressure     0.12791E-04      15   0.22814E-03   0.12718E-01 0.86349E+01 
c  k            0.15591E-01      11   0.26330E-04   0.41087E-01 0.41558E+02 
c  omega        0.27922E+07       1   0.75398E-07   0.15050E+08 0.60434E+00 
c  TempK        0.10099E+05       5   0.43821E-05   0.10237E+02 0.11094E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6853e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.102       0.0016656      -0.0088072
v  Velocity[Y]             -15.663          14.924         0.18066         0.26467
v  Velocity[Z]             -25.447            12.2         -1.6511        -0.50737
v  ǁVelocityǁ         9.769e-005          25.623          7.7422          6.7147
v  Pressure                -520.95           202.1          25.162          28.733
v  k                   9.9164e-011           7.736         0.19015         0.40044
v  omega                    57.484     2.7322e+008     1.2912e+006           76899
v  TempK                    298.52          363.17          335.79          343.05
v  TurbVisc             2.485e-018       0.0012996     4.6723e-005       0.0001669
v  CourantNb            0.00015069          1.4958         0.79389         0.97554
v  FourierNb             0.0037693               1         0.40587         0.14972
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.003199      7.336e-005      0.00019833

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.3          306.42
v  Yplus               0           2.922         0.63369         0.49072


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67599          2.0888          1.1998          1.1253


 INSTANT    0.627000000E-02   TIME STEP NUMBER             627
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924979E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11451E-01 0.46811E+01
   Friction velocity        uk    :  0.11451E-01 0.46771E+01
   Dimensionless distance   yplus :  0.77639E-02 0.29218E+01
   Friction thermal sca.    tstar :  0.12120E+01 0.22313E+03
   Rough dim-less th. sca.  tplus :  0.55000E-02 0.20699E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27724E+00      10   0.79845E-05   0.30277E+01 0.27694E+02 
c  Velocity[X]                                      0.12439E+01 
c  Velocity[Y]                                      0.78715E+00 
c  Velocity[Z]                                      0.99660E+00 
c  Pressure     0.13109E-04      15   0.23069E-03   0.13037E-01 0.84477E+01 
c  k            0.15613E-01      11   0.26652E-04   0.41498E-01 0.41678E+02 
c  omega        0.27922E+07       1   0.75217E-07   0.15326E+08 0.61464E+00 
c  TempK        0.10100E+05       5   0.43717E-05   0.10196E+02 0.11072E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6854e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.252          19.101       0.0018158      -0.0088051
v  Velocity[Y]             -15.587          14.924         0.18106         0.26526
v  Velocity[Z]             -25.446            12.2          -1.651        -0.50737
v  ǁVelocityǁ        9.2239e-005          25.622          7.7419          6.7142
v  Pressure                -520.84          202.09          25.157          28.733
v  k                   9.9158e-011          7.8037         0.19038         0.40097
v  omega                    57.484     2.7322e+008     1.2912e+006           76899
v  TempK                    298.52          363.17           335.8          343.07
v  TurbVisc            2.4849e-018       0.0013035      4.678e-005      0.00016711
v  CourantNb            0.00015082          1.4958         0.79387         0.97554
v  FourierNb             0.0037695               1         0.40592         0.14985
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0032139     7.3363e-005      0.00019835

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.3          306.42
v  Yplus               0          2.9218         0.63366         0.49069


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68689          2.0888          1.1998          1.1254


 INSTANT    0.628000000E-02   TIME STEP NUMBER             628
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925090E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11087E-01 0.46811E+01
   Friction velocity        uk    :  0.11087E-01 0.46771E+01
   Dimensionless distance   yplus :  0.75171E-02 0.29218E+01
   Friction thermal sca.    tstar :  0.12119E+01 0.23046E+03
   Rough dim-less th. sca.  tplus :  0.53252E-02 0.20698E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27723E+00      10   0.80871E-05   0.30360E+01 0.27690E+02 
c  Velocity[X]                                      0.12479E+01 
c  Velocity[Y]                                      0.78561E+00 
c  Velocity[Z]                                      0.10025E+01 
c  Pressure     0.13052E-04      15   0.23113E-03   0.12982E-01 0.86255E+01 
c  k            0.15635E-01      11   0.27016E-04   0.41859E-01 0.41766E+02 
c  omega        0.27922E+07       1   0.73816E-07   0.12471E+08 0.56202E+00 
c  TempK        0.10100E+05       5   0.43612E-05   0.10155E+02 0.11051E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6856e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.251          19.101       0.0019653      -0.0088032
v  Velocity[Y]             -15.524          14.925         0.18146         0.26585
v  Velocity[Z]             -25.445          12.199          -1.651        -0.50737
v  ǁVelocityǁ        8.6515e-005           25.62          7.7415          6.7137
v  Pressure                -520.73          202.08          25.143          28.725
v  k                   9.9153e-011          7.8656         0.19061          0.4015
v  omega                    57.484     2.7322e+008     1.2912e+006           76899
v  TempK                    298.51          363.17          335.82          343.09
v  TurbVisc            2.4848e-018       0.0013072     4.6838e-005      0.00016732
v  CourantNb            0.00015102          1.4958         0.79385         0.97554
v  FourierNb             0.0037697               1         0.40598         0.14997
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0032342     7.3367e-005      0.00019837

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.3          306.42
v  Yplus               0          2.9218         0.63364         0.49066


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64307          2.0888          1.1998          1.1255


 INSTANT    0.629000000E-02   TIME STEP NUMBER             629
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925262E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10690E-01 0.46811E+01
   Friction velocity        uk    :  0.10690E-01 0.46771E+01
   Dimensionless distance   yplus :  0.72482E-02 0.29217E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.23901E+03
   Rough dim-less th. sca.  tplus :  0.51347E-02 0.20697E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27721E+00      10   0.81377E-05   0.30500E+01 0.27760E+02 
c  Velocity[X]                                      0.12528E+01 
c  Velocity[Y]                                      0.78882E+00 
c  Velocity[Z]                                      0.10084E+01 
c  Pressure     0.13090E-04      15   0.23191E-03   0.13021E-01 0.86273E+01 
c  k            0.15657E-01      11   0.27438E-04   0.42365E-01 0.41930E+02 
c  omega        0.27922E+07       1   0.69931E-07   0.46241E+07 0.37758E+00 
c  TempK        0.10101E+05       5   0.43508E-05   0.10114E+02 0.11030E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6856e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.251            19.1       0.0021153      -0.0088016
v  Velocity[Y]             -15.492          14.926         0.18185         0.26645
v  Velocity[Z]             -25.443          12.198         -1.6509        -0.50737
v  ǁVelocityǁ         8.149e-005          25.619          7.7411          6.7131
v  Pressure                -520.62          202.06          25.131          28.719
v  k                   9.9147e-011          7.9163         0.19084         0.40203
v  omega                    57.484     2.7322e+008     1.2912e+006           76899
v  TempK                    298.51          363.17          335.83          343.12
v  TurbVisc            2.4846e-018       0.0013106     4.6894e-005      0.00016752
v  CourantNb            0.00015122          1.4958         0.79384         0.97553
v  FourierNb             0.0037699               1         0.40603         0.15009
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0032599      7.337e-005      0.00019839

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.3          306.42
v  Yplus               0          2.9217         0.63361         0.49063


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45641          2.0888          1.1999          1.1256


 INSTANT    0.630000000E-02   TIME STEP NUMBER             630
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925217E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10328E-01 0.46810E+01
   Friction velocity        uk    :  0.10328E-01 0.46771E+01
   Dimensionless distance   yplus :  0.70026E-02 0.29216E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.24739E+03
   Rough dim-less th. sca.  tplus :  0.49607E-02 0.20697E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27719E+00      10   0.81307E-05   0.30668E+01 0.27848E+02 
c  Velocity[X]                                      0.12582E+01 
c  Velocity[Y]                                      0.79408E+00 
c  Velocity[Z]                                      0.10146E+01 
c  Pressure     0.12981E-04      15   0.23795E-03   0.12915E-01 0.85013E+01 
c  k            0.15679E-01      11   0.27872E-04   0.42850E-01 0.42096E+02 
c  omega        0.27922E+07       1   0.69795E-07   0.42029E+07 0.36993E+00 
c  TempK        0.10101E+05       5   0.43404E-05   0.10070E+02 0.11010E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6852e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.25          19.099       0.0022639      -0.0088014
v  Velocity[Y]              -15.51          14.927         0.18225         0.26704
v  Velocity[Z]             -25.442          12.197         -1.6509        -0.50737
v  ǁVelocityǁ        7.6147e-005          25.618          7.7408          6.7126
v  Pressure                -520.51          202.05           25.12          28.714
v  k                   9.9142e-011          8.1538         0.19106         0.40255
v  omega                    57.484     2.7322e+008     1.2912e+006           76899
v  TempK                    298.51          363.17          335.84          343.14
v  TurbVisc            2.4845e-018       0.0013136     4.6951e-005      0.00016773
v  CourantNb            0.00011685          1.4958         0.79382         0.97553
v  FourierNb             0.0037701               1         0.40609         0.15021
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0032886     7.3373e-005       0.0001984

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.3          306.42
v  Yplus               0          2.9216         0.63359          0.4906


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69273          2.0889          1.1999          1.1257


 INSTANT    0.631000000E-02   TIME STEP NUMBER             631
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925094E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99265E-02 0.46810E+01
   Friction velocity        uk    :  0.99264E-02 0.46770E+01
   Dimensionless distance   yplus :  0.67303E-02 0.29215E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.25740E+03
   Rough dim-less th. sca.  tplus :  0.47678E-02 0.20696E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27718E+00      10   0.81656E-05   0.30845E+01 0.27940E+02 
c  Velocity[X]                                      0.12632E+01 
c  Velocity[Y]                                      0.79877E+00 
c  Velocity[Z]                                      0.10225E+01 
c  Pressure     0.13118E-04      15   0.23595E-03   0.13053E-01 0.84420E+01 
c  k            0.15701E-01      11   0.28334E-04   0.43229E-01 0.42175E+02 
c  omega        0.27922E+07       1   0.71836E-07   0.74640E+07 0.45592E+00 
c  TempK        0.10101E+05       5   0.43299E-05   0.10026E+02 0.10990E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6844e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.249          19.099       0.0024107      -0.0088021
v  Velocity[Y]             -15.574          14.929         0.18264         0.26764
v  Velocity[Z]             -25.441          12.196         -1.6509        -0.50737
v  ǁVelocityǁ        7.0926e-005          25.617          7.7404           6.712
v  Pressure                -520.39          202.04          25.115          28.714
v  k                   9.9137e-011          7.9585         0.19129         0.40307
v  omega                    57.484     2.7322e+008     1.2912e+006           76899
v  TempK                    298.51          363.17          335.86          343.16
v  TurbVisc            2.4844e-018       0.0013162     4.7008e-005      0.00016793
v  CourantNb           8.9022e-005           1.496         0.79381         0.97553
v  FourierNb             0.0037703               1         0.40614         0.15034
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0033241     7.3377e-005      0.00019842

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.3          306.42
v  Yplus               0          2.9215         0.63357         0.49057


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5393          2.0891             1.2          1.1259


 INSTANT    0.632000000E-02   TIME STEP NUMBER             632
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924953E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95152E-02 0.46810E+01
   Friction velocity        uk    :  0.95152E-02 0.46770E+01
   Dimensionless distance   yplus :  0.64515E-02 0.29215E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.26853E+03
   Rough dim-less th. sca.  tplus :  0.45703E-02 0.20696E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27716E+00      10   0.82236E-05   0.31049E+01 0.28066E+02 
c  Velocity[X]                                      0.12683E+01 
c  Velocity[Y]                                      0.80515E+00 
c  Velocity[Z]                                      0.10315E+01 
c  Pressure     0.12749E-04      15   0.24111E-03   0.12688E-01 0.85588E+01 
c  k            0.15722E-01      11   0.28677E-04   0.43767E-01 0.42352E+02 
c  omega        0.27922E+07       1   0.74592E-07   0.11817E+08 0.54946E+00 
c  TempK        0.10102E+05       5   0.43195E-05   0.99850E+01 0.10971E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6834e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.248          19.098       0.0025556      -0.0088043
v  Velocity[Y]             -15.636          14.929         0.18304         0.26824
v  Velocity[Z]              -25.44          12.195         -1.6509        -0.50738
v  ǁVelocityǁ        6.5098e-005          25.616          7.7401          6.7115
v  Pressure                -520.27          202.04          25.113          28.717
v  k                   9.9131e-011          7.9495         0.19152         0.40359
v  omega                    57.484     2.7322e+008     1.2912e+006           76899
v  TempK                    298.51          363.17          335.87          343.19
v  TurbVisc            2.4842e-018       0.0013185     4.7064e-005      0.00016813
v  CourantNb           6.3339e-005          1.4962         0.79379         0.97552
v  FourierNb             0.0037705               1          0.4062         0.15046
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.003366     7.3381e-005      0.00019844

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.31          306.42
v  Yplus               0          2.9215         0.63354         0.49054


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45402          2.0894             1.2           1.126


 INSTANT    0.633000000E-02   TIME STEP NUMBER             633
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924678E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.90317E-02 0.46810E+01
   Friction velocity        uk    :  0.90317E-02 0.46770E+01
   Dimensionless distance   yplus :  0.61237E-02 0.29214E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.28290E+03
   Rough dim-less th. sca.  tplus :  0.43380E-02 0.20695E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27715E+00      10   0.82697E-05   0.31308E+01 0.28232E+02 
c  Velocity[X]                                      0.12748E+01 
c  Velocity[Y]                                      0.81700E+00 
c  Velocity[Z]                                      0.10390E+01 
c  Pressure     0.13075E-04      15   0.23395E-03   0.13014E-01 0.87742E+01 
c  k            0.15744E-01      11   0.29079E-04   0.44358E-01 0.42529E+02 
c  omega        0.27922E+07       1   0.75837E-07   0.14195E+08 0.59860E+00 
c  TempK        0.10102E+05       5   0.43090E-05   0.99445E+01 0.10952E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6833e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.246          19.097       0.0026981      -0.0088081
v  Velocity[Y]             -15.592           14.93         0.18343         0.26885
v  Velocity[Z]             -25.439          12.194         -1.6509        -0.50738
v  ǁVelocityǁ        5.9036e-005          25.615          7.7397           6.711
v  Pressure                -520.15          202.03          25.115          28.724
v  k                   9.9126e-011           7.923         0.19174          0.4041
v  omega                    57.484     2.7322e+008     1.2912e+006           76899
v  TempK                    298.51          363.17          335.88          343.21
v  TurbVisc            2.4841e-018       0.0013149     4.7121e-005      0.00016833
v  CourantNb           6.4887e-005          1.4963         0.79377         0.97552
v  FourierNb             0.0037706               1         0.40626         0.15058
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0033537     7.3385e-005      0.00019846

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.31          306.43
v  Yplus               0          2.9214         0.63352         0.49051


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48618          2.0894             1.2          1.1261


 INSTANT    0.634000000E-02   TIME STEP NUMBER             634
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924340E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84940E-02 0.46809E+01
   Friction velocity        uk    :  0.84940E-02 0.46769E+01
   Dimensionless distance   yplus :  0.57591E-02 0.29213E+01
   Friction thermal sca.    tstar :  0.12120E+01 0.30081E+03
   Rough dim-less th. sca.  tplus :  0.40798E-02 0.20695E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27713E+00      10   0.82963E-05   0.31448E+01 0.28295E+02 
c  Velocity[X]                                      0.12816E+01 
c  Velocity[Y]                                      0.81873E+00 
c  Velocity[Z]                                      0.10445E+01 
c  Pressure     0.12978E-04      15   0.23824E-03   0.12919E-01 0.86038E+01 
c  k            0.15765E-01      11   0.29465E-04   0.44815E-01 0.42626E+02 
c  omega        0.27922E+07       1   0.74601E-07   0.11506E+08 0.54927E+00 
c  TempK        0.10103E+05       5   0.42987E-05   0.99038E+01 0.10932E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6833e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.245          19.097       0.0028375      -0.0088128
v  Velocity[Y]              -15.49          14.932         0.18382         0.26945
v  Velocity[Z]             -25.438          12.193         -1.6508        -0.50739
v  ǁVelocityǁ        5.3007e-005          25.614          7.7393          6.7104
v  Pressure                -520.04          202.03          25.115          28.729
v  k                   9.9121e-011          7.8837         0.19197         0.40461
v  omega                    57.484     2.7322e+008     1.2912e+006           76899
v  TempK                    298.51          363.17           335.9          343.24
v  TurbVisc             2.484e-018       0.0013099     4.7177e-005      0.00016852
v  CourantNb           8.6089e-005          1.4963         0.79376         0.97551
v  FourierNb             0.0037708               1         0.40631          0.1507
v  total_pressure       1.008e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.003689      7.339e-005      0.00019848

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.31          306.43
v  Yplus               0          2.9213         0.63349         0.49048


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75237          2.0894          1.2001          1.1262


 INSTANT    0.635000000E-02   TIME STEP NUMBER             635
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924459E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.79165E-02 0.46809E+01
   Friction velocity        uk    :  0.79165E-02 0.46769E+01
   Dimensionless distance   yplus :  0.53675E-02 0.29212E+01
   Friction thermal sca.    tstar :  0.12119E+01 0.32276E+03
   Rough dim-less th. sca.  tplus :  0.38024E-02 0.20694E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27712E+00      10   0.83340E-05   0.31605E+01 0.28356E+02 
c  Velocity[X]                                      0.12866E+01 
c  Velocity[Y]                                      0.82176E+00 
c  Velocity[Z]                                      0.10522E+01 
c  Pressure     0.13314E-04      15   0.24100E-03   0.13255E-01 0.86193E+01 
c  k            0.15786E-01      11   0.29931E-04   0.45399E-01 0.42790E+02 
c  omega        0.27922E+07       1   0.73179E-07   0.83967E+07 0.48696E+00 
c  TempK        0.10103E+05       5   0.42883E-05   0.98625E+01 0.10913E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6831e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.244          19.096       0.0029726      -0.0088173
v  Velocity[Y]             -15.453          14.933         0.18422         0.27006
v  Velocity[Z]             -25.437          12.192         -1.6508        -0.50739
v  ǁVelocityǁ         4.656e-005          25.612          7.7389          6.7099
v  Pressure                -519.93          202.02          25.112          28.732
v  k                   9.9116e-011          7.8173         0.19219         0.40512
v  omega                    57.484     2.7322e+008     1.2912e+006           76898
v  TempK                    298.51          363.17          335.91          343.26
v  TurbVisc            2.4838e-018       0.0013046     4.7233e-005      0.00016872
v  CourantNb            0.00011311          1.4963         0.79374         0.97551
v  FourierNb              0.003771               1         0.40637         0.15082
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.004058     7.3394e-005       0.0001985

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.31          306.43
v  Yplus               0          2.9212         0.63347         0.49045


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72108          2.0895          1.2001          1.1263


 INSTANT    0.636000000E-02   TIME STEP NUMBER             636
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924862E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72379E-02 0.46809E+01
   Friction velocity        uk    :  0.72379E-02 0.46769E+01
   Dimensionless distance   yplus :  0.49074E-02 0.29211E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.35302E+03
   Rough dim-less th. sca.  tplus :  0.34764E-02 0.20694E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27710E+00      10   0.83747E-05   0.31751E+01 0.28430E+02 
c  Velocity[X]                                      0.12922E+01 
c  Velocity[Y]                                      0.82504E+00 
c  Velocity[Z]                                      0.10579E+01 
c  Pressure     0.13215E-04      15   0.24662E-03   0.13158E-01 0.85670E+01 
c  k            0.15808E-01      11   0.30400E-04   0.45978E-01 0.42957E+02 
c  omega        0.27922E+07       1   0.71912E-07   0.48026E+07 0.40107E+00 
c  TempK        0.10104E+05       5   0.42779E-05   0.98215E+01 0.10894E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6826e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.242          19.095        0.003103       -0.008824
v  Velocity[Y]             -15.475          14.934         0.18461         0.27066
v  Velocity[Z]             -25.436           12.19         -1.6508        -0.50739
v  ǁVelocityǁ        4.1009e-005          25.611          7.7386          6.7094
v  Pressure                -519.82          202.02          25.108          28.734
v  k                   9.9111e-011          7.7816         0.19241         0.40563
v  omega                    57.484     2.7322e+008     1.2912e+006           76898
v  TempK                    298.51          363.17          335.92          343.28
v  TurbVisc            2.4837e-018        0.001299     4.7288e-005      0.00016892
v  CourantNb            0.00015274          1.4964         0.79373          0.9755
v  FourierNb             0.0037712               1         0.40642         0.15094
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0041509     7.3397e-005      0.00019852

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.31          306.43
v  Yplus               0          2.9211         0.63344         0.49043


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7117          2.0896          1.2002          1.1264


 INSTANT    0.637000000E-02   TIME STEP NUMBER             637
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925089E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65781E-02 0.46808E+01
   Friction velocity        uk    :  0.65780E-02 0.46768E+01
   Dimensionless distance   yplus :  0.44600E-02 0.29211E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.38843E+03
   Rough dim-less th. sca.  tplus :  0.31595E-02 0.20693E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27709E+00      10   0.84122E-05   0.31907E+01 0.28522E+02 
c  Velocity[X]                                      0.12972E+01 
c  Velocity[Y]                                      0.82953E+00 
c  Velocity[Z]                                      0.10640E+01 
c  Pressure     0.13289E-04      15   0.24248E-03   0.13233E-01 0.87974E+01 
c  k            0.15829E-01      11   0.30882E-04   0.46467E-01 0.43060E+02 
c  omega        0.27922E+07       1   0.74111E-07   0.82542E+07 0.48899E+00 
c  TempK        0.10104E+05       5   0.42675E-05   0.97813E+01 0.10876E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6816e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.241          19.095       0.0032295        -0.00883
v  Velocity[Y]              -15.55          14.936         0.18499         0.27127
v  Velocity[Z]             -25.435          12.189         -1.6508        -0.50739
v  ǁVelocityǁ        3.4316e-005           25.61          7.7382          6.7088
v  Pressure                 -519.7          202.01          25.101          28.733
v  k                   9.9106e-011          7.6082         0.19264         0.40614
v  omega                    57.484     2.7322e+008     1.2912e+006           76898
v  TempK                    298.51          363.17          335.94          343.31
v  TurbVisc            2.4836e-018       0.0012934     4.7344e-005      0.00016911
v  CourantNb            0.00015297          1.4966         0.79372          0.9755
v  FourierNb             0.0037714               1         0.40648         0.15106
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0041429     7.3402e-005      0.00019854

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.31          306.43
v  Yplus               0          2.9211         0.63342          0.4904


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60762          2.0899          1.2002          1.1266


 INSTANT    0.638000000E-02   TIME STEP NUMBER             638
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924929E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.56642E-02 0.46808E+01
   Friction velocity        uk    :  0.56641E-02 0.46768E+01
   Dimensionless distance   yplus :  0.38404E-02 0.29210E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.45110E+03
   Rough dim-less th. sca.  tplus :  0.27206E-02 0.20693E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27707E+00      10   0.84549E-05   0.32101E+01 0.28646E+02 
c  Velocity[X]                                      0.13026E+01 
c  Velocity[Y]                                      0.83524E+00 
c  Velocity[Z]                                      0.10722E+01 
c  Pressure     0.13202E-04      15   0.24089E-03   0.13147E-01 0.88136E+01 
c  k            0.15850E-01      11   0.31329E-04   0.47058E-01 0.43231E+02 
c  omega        0.27922E+07       1   0.75667E-07   0.10260E+08 0.53122E+00 
c  TempK        0.10104E+05       5   0.42570E-05   0.97406E+01 0.10859E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6805e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.241          19.094       0.0033544      -0.0088361
v  Velocity[Y]             -15.617          14.937         0.18537         0.27187
v  Velocity[Z]             -25.434          12.188         -1.6508         -0.5074
v  ǁVelocityǁ        3.0522e-005           25.61          7.7378          6.7083
v  Pressure                -519.58             202          25.102          28.738
v  k                   9.9101e-011          7.4633         0.19286         0.40664
v  omega                    57.484     2.7322e+008     1.2912e+006           76898
v  TempK                    298.51          363.17          335.95          343.33
v  TurbVisc            2.4834e-018       0.0012877       4.74e-005       0.0001693
v  CourantNb            0.00015331          1.4969          0.7937         0.97549
v  FourierNb             0.0037716               1         0.40653         0.15119
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040714     7.3407e-005      0.00019856

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.31          306.43
v  Yplus               0           2.921          0.6334         0.49037


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66609          2.0901          1.2002          1.1267


 INSTANT    0.639000000E-02   TIME STEP NUMBER             639
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924445E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.50596E-02 0.46807E+01
   Friction velocity        uk    :  0.50595E-02 0.46768E+01
   Dimensionless distance   yplus :  0.34305E-02 0.29210E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.50501E+03
   Rough dim-less th. sca.  tplus :  0.24302E-02 0.20692E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27706E+00      10   0.84889E-05   0.32290E+01 0.28774E+02 
c  Velocity[X]                                      0.13070E+01 
c  Velocity[Y]                                      0.84292E+00 
c  Velocity[Z]                                      0.10791E+01 
c  Pressure     0.13069E-04      15   0.24083E-03   0.13015E-01 0.91036E+01 
c  k            0.15871E-01      11   0.31731E-04   0.47689E-01 0.43427E+02 
c  omega        0.27922E+07       1   0.76434E-07   0.12206E+08 0.57339E+00 
c  TempK        0.10105E+05       5   0.42466E-05   0.96995E+01 0.10840E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6802e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.241          19.093        0.003474      -0.0088426
v  Velocity[Y]             -15.585          14.938         0.18575         0.27247
v  Velocity[Z]             -25.434          12.187         -1.6508        -0.50741
v  ǁVelocityǁ        2.6436e-005          25.609          7.7375          6.7077
v  Pressure                -519.46          202.01          25.112          28.754
v  k                   9.9096e-011          7.2953         0.19308         0.40715
v  omega                    57.483     2.7322e+008     1.2912e+006           76898
v  TempK                     298.5          363.17          335.96          343.35
v  TurbVisc            2.4833e-018        0.001282     4.7455e-005      0.00016949
v  CourantNb            0.00015351           1.497         0.79369         0.97549
v  FourierNb             0.0037718               1         0.40658         0.15131
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.004084     7.3412e-005      0.00019858

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.32          306.43
v  Yplus               0           2.921         0.63338         0.49035


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71817          2.0902          1.2003          1.1268


 INSTANT    0.640000000E-02   TIME STEP NUMBER             640
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924064E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44695E-02 0.46807E+01
   Friction velocity        uk    :  0.44695E-02 0.46767E+01
   Dimensionless distance   yplus :  0.30304E-02 0.29209E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.57168E+03
   Rough dim-less th. sca.  tplus :  0.21468E-02 0.20692E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27704E+00      10   0.85272E-05   0.32426E+01 0.28844E+02 
c  Velocity[X]                                      0.13107E+01 
c  Velocity[Y]                                      0.84591E+00 
c  Velocity[Z]                                      0.10859E+01 
c  Pressure     0.12908E-04      16   0.24173E-03   0.12856E-01 0.93392E+01 
c  k            0.15892E-01      11   0.32236E-04   0.48186E-01 0.43532E+02 
c  omega        0.27922E+07       1   0.77363E-07   0.13248E+08 0.59116E+00 
c  TempK        0.10105E+05       5   0.42362E-05   0.96587E+01 0.10820E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6801e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.241          19.093       0.0035909       -0.008851
v  Velocity[Y]              -15.49           14.94         0.18614         0.27308
v  Velocity[Z]             -25.433          12.185         -1.6508        -0.50741
v  ǁVelocityǁ        2.5165e-005          25.608          7.7371          6.7072
v  Pressure                -519.34          202.02          25.126          28.773
v  k                   9.9091e-011          7.1088          0.1933         0.40765
v  omega                    57.483     2.7322e+008     1.2912e+006           76898
v  TempK                     298.5          363.17          335.98          343.37
v  TurbVisc            2.4832e-018       0.0012763     4.7511e-005      0.00016968
v  CourantNb            0.00015385           1.497         0.79367         0.97548
v  FourierNb             0.0037721               1         0.40664         0.15143
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040489     7.3417e-005      0.00019861

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.32          306.43
v  Yplus               0          2.9209         0.63336         0.49032


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.79895          2.0903          1.2003          1.1269


 INSTANT    0.641000000E-02   TIME STEP NUMBER             641
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923946E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47327E-02 0.46807E+01
   Friction velocity        uk    :  0.47327E-02 0.46767E+01
   Dimensionless distance   yplus :  0.32088E-02 0.29208E+01
   Friction thermal sca.    tstar :  0.12120E+01 0.53989E+03
   Rough dim-less th. sca.  tplus :  0.22732E-02 0.20691E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27703E+00      10   0.85775E-05   0.32540E+01 0.28904E+02 
c  Velocity[X]                                      0.13142E+01 
c  Velocity[Y]                                      0.84905E+00 
c  Velocity[Z]                                      0.10908E+01 
c  Pressure     0.12973E-04      16   0.23846E-03   0.12922E-01 0.89976E+01 
c  k            0.15913E-01      11   0.32858E-04   0.48766E-01 0.43677E+02 
c  omega        0.27922E+07       1   0.75257E-07   0.85690E+07 0.49799E+00 
c  TempK        0.10106E+05       5   0.42259E-05   0.96190E+01 0.10801E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6798e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.241          19.092       0.0037027       -0.008861
v  Velocity[Y]             -15.459          14.941         0.18653         0.27369
v  Velocity[Z]             -25.432          12.184         -1.6507        -0.50742
v  ǁVelocityǁ        2.7123e-005          25.607          7.7367          6.7066
v  Pressure                -519.22          202.03          25.133          28.787
v  k                   9.9086e-011           7.134         0.19352         0.40815
v  omega                    57.483     2.7322e+008     1.2912e+006           76898
v  TempK                     298.5          363.17          335.99           343.4
v  TurbVisc            2.4831e-018       0.0012707     4.7567e-005      0.00016987
v  CourantNb            0.00015418          1.4971         0.79366         0.97547
v  FourierNb             0.0037723               1         0.40669         0.15155
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040125     7.3422e-005      0.00019863

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.32          306.43
v  Yplus               0          2.9208         0.63333          0.4903


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74184          2.0904          1.2004           1.127


 INSTANT    0.642000000E-02   TIME STEP NUMBER             642
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923965E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.55686E-02 0.46806E+01
   Friction velocity        uk    :  0.55686E-02 0.46766E+01
   Dimensionless distance   yplus :  0.37756E-02 0.29208E+01
   Friction thermal sca.    tstar :  0.12119E+01 0.45884E+03
   Rough dim-less th. sca.  tplus :  0.26747E-02 0.20691E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27702E+00      10   0.86281E-05   0.32628E+01 0.28940E+02 
c  Velocity[X]                                      0.13164E+01 
c  Velocity[Y]                                      0.85144E+00 
c  Velocity[Z]                                      0.10950E+01 
c  Pressure     0.12904E-04      15   0.24122E-03   0.12855E-01 0.88291E+01 
c  k            0.15934E-01      11   0.33349E-04   0.49342E-01 0.43818E+02 
c  omega        0.27922E+07       1   0.75256E-07   0.85819E+07 0.50181E+00 
c  TempK        0.10106E+05       5   0.42156E-05   0.95811E+01 0.10781E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6791e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.24          19.091       0.0038123       -0.008869
v  Velocity[Y]             -15.483          14.943         0.18692         0.27429
v  Velocity[Z]             -25.431          12.183         -1.6507        -0.50743
v  ǁVelocityǁ        3.1401e-005          25.606          7.7364          6.7061
v  Pressure                 -519.1          202.03          25.138          28.797
v  k                   9.9081e-011          7.5293         0.19374         0.40866
v  omega                    57.483     2.7322e+008     1.2912e+006           76898
v  TempK                     298.5          363.17             336          343.42
v  TurbVisc            2.4829e-018        0.001265     4.7623e-005      0.00017006
v  CourantNb            0.00015451          1.4972         0.79364         0.97547
v  FourierNb             0.0037725               1         0.40675         0.15167
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0039748     7.3426e-005      0.00019865

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.32          306.43
v  Yplus               0          2.9208         0.63331         0.49028


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76414          2.0905          1.2004          1.1271


 INSTANT    0.643000000E-02   TIME STEP NUMBER             643
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924060E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64500E-02 0.46806E+01
   Friction velocity        uk    :  0.64500E-02 0.46766E+01
   Dimensionless distance   yplus :  0.43732E-02 0.29207E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.39614E+03
   Rough dim-less th. sca.  tplus :  0.30980E-02 0.20691E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27701E+00      10   0.86807E-05   0.32748E+01 0.28990E+02 
c  Velocity[X]                                      0.13202E+01 
c  Velocity[Y]                                      0.85406E+00 
c  Velocity[Z]                                      0.11005E+01 
c  Pressure     0.13115E-04      15   0.24046E-03   0.13067E-01 0.90768E+01 
c  k            0.15955E-01      11   0.33905E-04   0.49862E-01 0.43910E+02 
c  omega        0.27922E+07       1   0.75997E-07   0.87721E+07 0.50556E+00 
c  TempK        0.10107E+05       5   0.42053E-05   0.95425E+01 0.10763E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6779e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.24           19.09       0.0039194      -0.0088745
v  Velocity[Y]             -15.558          14.945          0.1873          0.2749
v  Velocity[Z]              -25.43          12.181         -1.6507        -0.50744
v  ǁVelocityǁ        3.7539e-005          25.606           7.736          6.7055
v  Pressure                -518.98          202.04          25.149          28.813
v  k                   9.9076e-011          7.5031         0.19396         0.40916
v  omega                    57.483     2.7322e+008     1.2912e+006           76898
v  TempK                     298.5          363.17          336.02          343.44
v  TurbVisc            2.4828e-018       0.0012624     4.7678e-005      0.00017025
v  CourantNb             0.0001548          1.4975         0.79363         0.97546
v  FourierNb             0.0037727               1          0.4068          0.1518
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.003936     7.3431e-005      0.00019868

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.32          306.44
v  Yplus               0          2.9207         0.63329         0.49025


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74875          2.0908          1.2004          1.1273


 INSTANT    0.644000000E-02   TIME STEP NUMBER             644
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924088E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.73255E-02 0.46805E+01
   Friction velocity        uk    :  0.73255E-02 0.46766E+01
   Dimensionless distance   yplus :  0.49668E-02 0.29207E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.34880E+03
   Rough dim-less th. sca.  tplus :  0.35185E-02 0.20690E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27699E+00      10   0.87370E-05   0.32896E+01 0.29075E+02 
c  Velocity[X]                                      0.13231E+01 
c  Velocity[Y]                                      0.85920E+00 
c  Velocity[Z]                                      0.11073E+01 
c  Pressure     0.12973E-04      16   0.24907E-03   0.12926E-01 0.93021E+01 
c  k            0.15976E-01      11   0.34523E-04   0.50517E-01 0.44074E+02 
c  omega        0.27922E+07       1   0.77474E-07   0.10473E+08 0.54291E+00 
c  TempK        0.10107E+05       5   0.41949E-05   0.95037E+01 0.10744E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6767e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.24           19.09       0.0040224       -0.008879
v  Velocity[Y]             -15.621          14.946         0.18769         0.27551
v  Velocity[Z]              -25.43           12.18         -1.6507        -0.50745
v  ǁVelocityǁ        4.3564e-005          25.605          7.7356          6.7049
v  Pressure                -518.85          202.04          25.163          28.833
v  k                   9.9071e-011          7.5863         0.19419         0.40966
v  omega                    57.483     2.7322e+008     1.2912e+006           76898
v  TempK                     298.5          363.17          336.03          343.47
v  TurbVisc            2.4827e-018       0.0012631     4.7735e-005      0.00017044
v  CourantNb            0.00015511          1.4978         0.79361         0.97545
v  FourierNb             0.0037729               1         0.40686         0.15192
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0038966     7.3435e-005       0.0001987

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.32          306.44
v  Yplus               0          2.9207         0.63327         0.49023


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76244          2.0911          1.2005          1.1274


 INSTANT    0.645000000E-02   TIME STEP NUMBER             645
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924030E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80194E-02 0.46805E+01
   Friction velocity        uk    :  0.80194E-02 0.46765E+01
   Dimensionless distance   yplus :  0.54373E-02 0.29206E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.31862E+03
   Rough dim-less th. sca.  tplus :  0.38518E-02 0.20690E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27698E+00      10   0.87829E-05   0.33052E+01 0.29163E+02 
c  Velocity[X]                                      0.13253E+01 
c  Velocity[Y]                                      0.86666E+00 
c  Velocity[Z]                                      0.11133E+01 
c  Pressure     0.13133E-04      16   0.24537E-03   0.13086E-01 0.95484E+01 
c  k            0.15997E-01      11   0.35019E-04   0.51210E-01 0.44240E+02 
c  omega        0.27922E+07       1   0.77241E-07   0.10275E+08 0.54427E+00 
c  TempK        0.10107E+05       5   0.41846E-05   0.94584E+01 0.10724E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6762e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.24          19.089       0.0041206      -0.0088806
v  Velocity[Y]             -15.588          14.948         0.18807         0.27612
v  Velocity[Z]             -25.429          12.178         -1.6507        -0.50746
v  ǁVelocityǁ        5.2035e-005          25.605          7.7353          6.7044
v  Pressure                -518.72          202.05           25.18          28.856
v  k                   9.9066e-011          7.6108         0.19441         0.41016
v  omega                    57.483     2.7322e+008     1.2912e+006           76898
v  TempK                     298.5          363.17          336.04          343.49
v  TurbVisc            2.4826e-018       0.0012652     4.7791e-005      0.00017062
v  CourantNb            0.00015535          1.4979          0.7936         0.97545
v  FourierNb             0.0037731               1         0.40691         0.15205
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0038578      7.344e-005      0.00019873

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.32          306.44
v  Yplus               0          2.9206         0.63326          0.4902


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73283          2.0912          1.2005          1.1275


 INSTANT    0.646000000E-02   TIME STEP NUMBER             646
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923989E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88540E-02 0.46804E+01
   Friction velocity        uk    :  0.88540E-02 0.46765E+01
   Dimensionless distance   yplus :  0.60032E-02 0.29206E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.28859E+03
   Rough dim-less th. sca.  tplus :  0.42527E-02 0.20690E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27697E+00      10   0.88348E-05   0.33110E+01 0.29183E+02 
c  Velocity[X]                                      0.13270E+01 
c  Velocity[Y]                                      0.86712E+00 
c  Velocity[Z]                                      0.11169E+01 
c  Pressure     0.13104E-04      18   0.24499E-03   0.13059E-01 0.94906E+01 
c  k            0.16018E-01      11   0.35591E-04   0.51847E-01 0.44366E+02 
c  omega        0.27922E+07       1   0.77976E-07   0.11354E+08 0.56578E+00 
c  TempK        0.10108E+05       5   0.41740E-05   0.94165E+01 0.10704E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6759e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.24          19.088       0.0042156      -0.0088797
v  Velocity[Y]             -15.493           14.95         0.18846         0.27673
v  Velocity[Z]             -25.429          12.177         -1.6507        -0.50747
v  ǁVelocityǁ        6.0789e-005          25.604          7.7349          6.7038
v  Pressure                 -518.6          202.07          25.197          28.879
v  k                   9.9062e-011          7.5868         0.19463         0.41066
v  omega                    57.483     2.7322e+008     1.2912e+006           76898
v  TempK                     298.5          363.17          336.05          343.51
v  TurbVisc            2.4825e-018       0.0012673     4.7847e-005      0.00017081
v  CourantNb             0.0001557          1.4979         0.79359         0.97544
v  FourierNb             0.0037733               1         0.40697         0.15217
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0038204     7.3445e-005      0.00019875

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.33          306.44
v  Yplus               0          2.9206         0.63324         0.49018


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69643          2.0913          1.2006          1.1276


 INSTANT    0.647000000E-02   TIME STEP NUMBER             647
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924051E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96126E-02 0.46804E+01
   Friction velocity        uk    :  0.96126E-02 0.46764E+01
   Dimensionless distance   yplus :  0.65175E-02 0.29205E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.26581E+03
   Rough dim-less th. sca.  tplus :  0.46170E-02 0.20689E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27695E+00      10   0.88747E-05   0.33260E+01 0.29260E+02 
c  Velocity[X]                                      0.13299E+01 
c  Velocity[Y]                                      0.87312E+00 
c  Velocity[Z]                                      0.11230E+01 
c  Pressure     0.12932E-04      16   0.25080E-03   0.12888E-01 0.97879E+01 
c  k            0.16039E-01      11   0.36269E-04   0.52610E-01 0.44551E+02 
c  omega        0.27922E+07       1   0.78114E-07   0.10272E+08 0.54545E+00 
c  TempK        0.10108E+05       5   0.41634E-05   0.93754E+01 0.10683E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6753e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.24          19.088       0.0043072      -0.0088771
v  Velocity[Y]             -15.462          14.952         0.18885         0.27734
v  Velocity[Z]             -25.428          12.175         -1.6507        -0.50747
v  ǁVelocityǁ        6.9281e-005          25.603          7.7346          6.7033
v  Pressure                -518.47          202.08          25.215          28.903
v  k                   9.9057e-011           7.525         0.19485         0.41117
v  omega                    57.483     2.7322e+008     1.2912e+006           76898
v  TempK                     298.5          363.17          336.07          343.53
v  TurbVisc            2.4823e-018       0.0012698     4.7903e-005      0.00017099
v  CourantNb            0.00015604          1.4981         0.79357         0.97543
v  FourierNb             0.0037736               1         0.40702          0.1523
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0037858     7.3449e-005      0.00019878

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.33          306.44
v  Yplus               0          2.9205         0.63322         0.49015


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63344          2.0914          1.2006          1.1277


 INSTANT    0.648000000E-02   TIME STEP NUMBER             648
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923878E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10280E-01 0.46803E+01
   Friction velocity        uk    :  0.10280E-01 0.46764E+01
   Dimensionless distance   yplus :  0.69699E-02 0.29205E+01
   Friction thermal sca.    tstar :  0.12120E+01 0.24856E+03
   Rough dim-less th. sca.  tplus :  0.49375E-02 0.20689E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27694E+00      10   0.89066E-05   0.33388E+01 0.29327E+02 
c  Velocity[X]                                      0.13336E+01 
c  Velocity[Y]                                      0.87745E+00 
c  Velocity[Z]                                      0.11277E+01 
c  Pressure     0.12991E-04      16   0.25194E-03   0.12948E-01 0.10029E+02 
c  k            0.16060E-01      11   0.36882E-04   0.53404E-01 0.44758E+02 
c  omega        0.27922E+07       1   0.77438E-07   0.86992E+07 0.51620E+00 
c  TempK        0.10109E+05       5   0.41528E-05   0.93340E+01 0.10662E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6744e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.239          19.087       0.0043957      -0.0088735
v  Velocity[Y]             -15.486          14.954         0.18924         0.27796
v  Velocity[Z]             -25.427          12.173         -1.6507        -0.50748
v  ǁVelocityǁ        7.9554e-005          25.603          7.7342          6.7027
v  Pressure                -518.34           202.1          25.238          28.932
v  k                   9.9052e-011          7.4336         0.19508         0.41167
v  omega                    57.483     2.7322e+008     1.2912e+006           76898
v  TempK                     298.5          363.17          336.08          343.56
v  TurbVisc            2.4822e-018       0.0012725      4.796e-005      0.00017118
v  CourantNb            0.00015634          1.4983         0.79356         0.97542
v  FourierNb             0.0037738               1         0.40708         0.15243
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0037395     7.3454e-005      0.00019881

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.33          306.44
v  Yplus               0          2.9205         0.63321         0.49013


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71438          2.0917          1.2006          1.1279


 INSTANT    0.649000000E-02   TIME STEP NUMBER             649
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923996E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11021E-01 0.46803E+01
   Friction velocity        uk    :  0.11021E-01 0.46763E+01
   Dimensionless distance   yplus :  0.74723E-02 0.29204E+01
   Friction thermal sca.    tstar :  0.12120E+01 0.23185E+03
   Rough dim-less th. sca.  tplus :  0.52934E-02 0.20688E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27693E+00      10   0.89829E-05   0.33495E+01 0.29372E+02 
c  Velocity[X]                                      0.13346E+01 
c  Velocity[Y]                                      0.88047E+00 
c  Velocity[Z]                                      0.11345E+01 
c  Pressure     0.12838E-04      16   0.25051E-03   0.12797E-01 0.97223E+01 
c  k            0.16081E-01      11   0.37395E-04   0.54127E-01 0.44915E+02 
c  omega        0.27922E+07       1   0.79329E-07   0.12575E+08 0.59499E+00 
c  TempK        0.10109E+05       5   0.41424E-05   0.92931E+01 0.10640E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6731e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.239          19.086       0.0044807      -0.0088682
v  Velocity[Y]             -15.561          14.956         0.18964         0.27857
v  Velocity[Z]             -25.427          12.172         -1.6507        -0.50748
v  ǁVelocityǁ        8.8045e-005          25.602          7.7338          6.7021
v  Pressure                -518.21           202.1          25.255          28.954
v  k                   9.9048e-011          7.3156          0.1953         0.41218
v  omega                    57.483     2.7322e+008     1.2912e+006           76897
v  TempK                     298.5          363.17          336.09          343.58
v  TurbVisc            2.4821e-018       0.0012748     4.8017e-005      0.00017137
v  CourantNb            0.00012673          1.4986         0.79354         0.97541
v  FourierNb              0.003774               1         0.40714         0.15256
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0036853     7.3458e-005      0.00019883

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.33          306.44
v  Yplus               0          2.9204         0.63319         0.49011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78276           2.092          1.2007           1.128


 INSTANT    0.650000000E-02   TIME STEP NUMBER             650
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923931E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11592E-01 0.46802E+01
   Friction velocity        uk    :  0.11592E-01 0.46762E+01
   Dimensionless distance   yplus :  0.78594E-02 0.29203E+01
   Friction thermal sca.    tstar :  0.12119E+01 0.22043E+03
   Rough dim-less th. sca.  tplus :  0.55676E-02 0.20688E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27692E+00      10   0.90312E-05   0.33630E+01 0.29443E+02 
c  Velocity[X]                                      0.13371E+01 
c  Velocity[Y]                                      0.88431E+00 
c  Velocity[Z]                                      0.11415E+01 
c  Pressure     0.12640E-04      16   0.24697E-03   0.12601E-01 0.10462E+02 
c  k            0.16103E-01      11   0.38056E-04   0.55022E-01 0.45128E+02 
c  omega        0.27922E+07       1   0.79289E-07   0.10873E+08 0.56269E+00 
c  TempK        0.10110E+05       5   0.41320E-05   0.92536E+01 0.10621E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6716e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.239          19.086       0.0045636        -0.00886
v  Velocity[Y]             -15.625          14.957         0.19003         0.27919
v  Velocity[Z]             -25.426           12.17         -1.6507        -0.50749
v  ǁVelocityǁ         9.806e-005          25.601          7.7334          6.7015
v  Pressure                -518.07          202.12          25.281          28.986
v  k                   9.9043e-011          7.1781         0.19553         0.41269
v  omega                    57.483     2.7322e+008     1.2912e+006           76897
v  TempK                     298.5          363.17          336.11           343.6
v  TurbVisc             2.482e-018       0.0012767     4.8074e-005      0.00017155
v  CourantNb            0.00010239          1.4989         0.79352          0.9754
v  FourierNb             0.0037743               1          0.4072         0.15269
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0036328     7.3463e-005      0.00019886

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.33          306.44
v  Yplus               0          2.9203         0.63317         0.49008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6742          2.0923          1.2007          1.1281


 INSTANT    0.651000000E-02   TIME STEP NUMBER             651
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923971E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12227E-01 0.46802E+01
   Friction velocity        uk    :  0.12227E-01 0.46762E+01
   Dimensionless distance   yplus :  0.82903E-02 0.29203E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.20897E+03
   Rough dim-less th. sca.  tplus :  0.58729E-02 0.20688E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27691E+00      10   0.90581E-05   0.33777E+01 0.29530E+02 
c  Velocity[X]                                      0.13399E+01 
c  Velocity[Y]                                      0.89069E+00 
c  Velocity[Z]                                      0.11471E+01 
c  Pressure     0.12453E-04      16   0.25245E-03   0.12416E-01 0.10376E+02 
c  k            0.16124E-01      11   0.38816E-04   0.55973E-01 0.45342E+02 
c  omega        0.27922E+07       1   0.78849E-07   0.10310E+08 0.55935E+00 
c  TempK        0.10110E+05       5   0.41214E-05   0.92131E+01 0.10599E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6709e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.239          19.085       0.0046428       -0.008849
v  Velocity[Y]             -15.593          14.959         0.19043          0.2798
v  Velocity[Z]             -25.426          12.168         -1.6507        -0.50751
v  ǁVelocityǁ         0.00010729          25.601          7.7331           6.701
v  Pressure                -517.93          202.14          25.306          29.017
v  k                   9.9038e-011          7.0246         0.19575          0.4132
v  omega                    57.483     2.7322e+008     1.2912e+006           76897
v  TempK                     298.5          363.17          336.12          343.62
v  TurbVisc            2.4819e-018       0.0012782     4.8131e-005      0.00017174
v  CourantNb           9.2063e-005           1.499         0.79351         0.97539
v  FourierNb             0.0037745               1         0.40726         0.15282
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0035847     7.3469e-005      0.00019889

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.33          306.44
v  Yplus               0          2.9203         0.63315         0.49006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75104          2.0925          1.2008          1.1282


 INSTANT    0.652000000E-02   TIME STEP NUMBER             652
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923982E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12782E-01 0.46801E+01
   Friction velocity        uk    :  0.12782E-01 0.46761E+01
   Dimensionless distance   yplus :  0.86663E-02 0.29203E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.19990E+03
   Rough dim-less th. sca.  tplus :  0.61393E-02 0.20687E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27689E+00      10   0.90947E-05   0.33822E+01 0.29539E+02 
c  Velocity[X]                                      0.13405E+01 
c  Velocity[Y]                                      0.88914E+00 
c  Velocity[Z]                                      0.11526E+01 
c  Pressure     0.12231E-04      16   0.25189E-03   0.12195E-01 0.10270E+02 
c  k            0.16146E-01      11   0.39653E-04   0.56800E-01 0.45494E+02 
c  omega        0.27922E+07       1   0.78829E-07   0.93342E+07 0.54462E+00 
c  TempK        0.10110E+05       5   0.41108E-05   0.91725E+01 0.10578E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6704e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.239          19.084       0.0047204      -0.0088357
v  Velocity[Y]             -15.499          14.962         0.19083         0.28042
v  Velocity[Z]             -25.426          12.166         -1.6507        -0.50752
v  ǁVelocityǁ          0.0001172          25.601          7.7327          6.7004
v  Pressure                -517.79          202.16          25.328          29.046
v  k                   9.9034e-011          6.8588         0.19597         0.41371
v  omega                    57.483     2.7322e+008     1.2912e+006           76897
v  TempK                     298.5          363.17          336.13          343.64
v  TurbVisc            2.4818e-018       0.0012794     4.8188e-005      0.00017192
v  CourantNb           9.0314e-005          1.4992         0.79349         0.97538
v  FourierNb             0.0037748               1         0.40732         0.15296
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0035419     7.3475e-005      0.00019891

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.33          306.44
v  Yplus               0          2.9203         0.63314         0.49004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.8177          2.0926          1.2008          1.1283


 INSTANT    0.653000000E-02   TIME STEP NUMBER             653
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923914E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13350E-01 0.46800E+01
   Friction velocity        uk    :  0.13350E-01 0.46761E+01
   Dimensionless distance   yplus :  0.90512E-02 0.29202E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.19140E+03
   Rough dim-less th. sca.  tplus :  0.64120E-02 0.20687E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27688E+00      10   0.91341E-05   0.33881E+01 0.29569E+02 
c  Velocity[X]                                      0.13404E+01 
c  Velocity[Y]                                      0.88981E+00 
c  Velocity[Z]                                      0.11578E+01 
c  Pressure     0.12294E-04      17   0.25466E-03   0.12259E-01 0.11162E+02 
c  k            0.16168E-01      11   0.40491E-04   0.57730E-01 0.45687E+02 
c  omega        0.27922E+07       1   0.78581E-07   0.79236E+07 0.51886E+00 
c  TempK        0.10111E+05       5   0.41003E-05   0.91334E+01 0.10558E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6697e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.238          19.084       0.0047925      -0.0088217
v  Velocity[Y]             -15.468          14.964         0.19123         0.28103
v  Velocity[Z]             -25.425          12.165         -1.6507        -0.50753
v  ǁVelocityǁ         0.00012691            25.6          7.7323          6.6998
v  Pressure                -517.65          202.18          25.362          29.086
v  k                   9.9029e-011          6.6919          0.1962         0.41422
v  omega                    57.483     2.7322e+008     1.2912e+006           76897
v  TempK                     298.5          363.17          336.14          343.67
v  TurbVisc            2.4816e-018       0.0012805     4.8246e-005      0.00017211
v  CourantNb           8.8306e-005          1.4993         0.79348         0.97538
v  FourierNb              0.003775               1         0.40738         0.15309
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0035029      7.348e-005      0.00019894

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.34          306.45
v  Yplus               0          2.9202         0.63312         0.49001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85096          2.0928          1.2009          1.1285


 INSTANT    0.654000000E-02   TIME STEP NUMBER             654
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924126E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13882E-01 0.46800E+01
   Friction velocity        uk    :  0.13882E-01 0.46760E+01
   Dimensionless distance   yplus :  0.94119E-02 0.29202E+01
   Friction thermal sca.    tstar :  0.12119E+01 0.18407E+03
   Rough dim-less th. sca.  tplus :  0.66675E-02 0.20687E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27687E+00      10   0.91688E-05   0.33970E+01 0.29630E+02 
c  Velocity[X]                                      0.13405E+01 
c  Velocity[Y]                                      0.89442E+00 
c  Velocity[Z]                                      0.11621E+01 
c  Pressure     0.12291E-04      17   0.25902E-03   0.12258E-01 0.11262E+02 
c  k            0.16190E-01      11   0.41307E-04   0.58698E-01 0.45904E+02 
c  omega        0.27922E+07       1   0.80221E-07   0.99553E+07 0.56468E+00 
c  TempK        0.10111E+05       5   0.40898E-05   0.90948E+01 0.10537E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6686e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.238          19.083       0.0048617      -0.0088034
v  Velocity[Y]             -15.492          14.966         0.19164         0.28164
v  Velocity[Z]             -25.425          12.163         -1.6507        -0.50754
v  ǁVelocityǁ         0.00013753            25.6           7.732          6.6992
v  Pressure                -517.51          202.21          25.396          29.126
v  k                   9.9025e-011          6.9091         0.19643         0.41474
v  omega                    57.483     2.7322e+008     1.2912e+006           76897
v  TempK                     298.5          363.17          336.15          343.69
v  TurbVisc            2.4815e-018       0.0012814     4.8303e-005      0.00017229
v  CourantNb             8.62e-005          1.4996         0.79346         0.97537
v  FourierNb             0.0037753               1         0.40744         0.15322
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0034692     7.3485e-005      0.00019897

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.34          306.45
v  Yplus               0          2.9202          0.6331         0.48999


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77286          2.0931          1.2009          1.1286


 INSTANT    0.655000000E-02   TIME STEP NUMBER             655
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924132E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14440E-01 0.46799E+01
   Friction velocity        uk    :  0.14440E-01 0.46759E+01
   Dimensionless distance   yplus :  0.97908E-02 0.29201E+01
   Friction thermal sca.    tstar :  0.12121E+01 0.17695E+03
   Rough dim-less th. sca.  tplus :  0.69358E-02 0.20686E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27685E+00      10   0.92521E-05   0.34048E+01 0.29669E+02 
c  Velocity[X]                                      0.13411E+01 
c  Velocity[Y]                                      0.89588E+00 
c  Velocity[Z]                                      0.11678E+01 
c  Pressure     0.12483E-04      17   0.25599E-03   0.12449E-01 0.11019E+02 
c  k            0.16212E-01      11   0.41969E-04   0.59617E-01 0.46102E+02 
c  omega        0.27922E+07       1   0.81534E-07   0.12308E+08 0.61130E+00 
c  TempK        0.10112E+05       5   0.40794E-05   0.90563E+01 0.10517E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.667e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.238          19.082       0.0049282      -0.0087832
v  Velocity[Y]             -15.567          14.969         0.19206         0.28226
v  Velocity[Z]             -25.424          12.161         -1.6507        -0.50755
v  ǁVelocityǁ         0.00014648          25.599          7.7316          6.6986
v  Pressure                -517.37          202.24          25.428          29.163
v  k                    9.902e-011          6.9181         0.19665         0.41525
v  omega                    57.483     2.7322e+008     1.2912e+006           76897
v  TempK                     298.5          363.17          336.17          343.71
v  TurbVisc            2.4814e-018       0.0012817     4.8361e-005      0.00017248
v  CourantNb            8.416e-005          1.4999         0.79345         0.97536
v  FourierNb             0.0037755               1          0.4075         0.15336
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0033688     7.3491e-005        0.000199

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.34          306.45
v  Yplus               0          2.9201         0.63309         0.48997


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74651          2.0934          1.2009          1.1287


 INSTANT    0.656000000E-02   TIME STEP NUMBER             656
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924116E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14703E-01 0.46798E+01
   Friction velocity        uk    :  0.14703E-01 0.46758E+01
   Dimensionless distance   yplus :  0.99692E-02 0.29201E+01
   Friction thermal sca.    tstar :  0.12121E+01 0.17184E+03
   Rough dim-less th. sca.  tplus :  0.70622E-02 0.20686E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27684E+00      10   0.92863E-05   0.34126E+01 0.29702E+02 
c  Velocity[X]                                      0.13397E+01 
c  Velocity[Y]                                      0.89777E+00 
c  Velocity[Z]                                      0.11752E+01 
c  Pressure     0.12309E-04      18   0.24799E-03   0.12276E-01 0.11281E+02 
c  k            0.16234E-01      11   0.42694E-04   0.60682E-01 0.46355E+02 
c  omega        0.27922E+07       1   0.82846E-07   0.14417E+08 0.65029E+00 
c  TempK        0.10112E+05       5   0.40688E-05   0.90174E+01 0.10496E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6654e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.237          19.081       0.0049936      -0.0087628
v  Velocity[Y]             -15.631          14.971         0.19247         0.28287
v  Velocity[Z]             -25.424          12.159         -1.6507        -0.50757
v  ǁVelocityǁ         0.00015636          25.599          7.7312           6.698
v  Pressure                -517.22          202.27          25.463          29.204
v  k                   9.9016e-011          6.7589         0.19688         0.41577
v  omega                    57.483     2.7322e+008     1.2912e+006           76897
v  TempK                     298.5          363.17          336.18          343.73
v  TurbVisc            2.4813e-018       0.0012818     4.8419e-005      0.00017266
v  CourantNb           8.4726e-005          1.5003         0.79343         0.97535
v  FourierNb             0.0037758               1         0.40756          0.1535
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0033371     7.3497e-005      0.00019903

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.34          306.45
v  Yplus               0          2.9201         0.63307         0.48994


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.84115          2.0938           1.201          1.1288


 INSTANT    0.657000000E-02   TIME STEP NUMBER             657
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924234E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14664E-01 0.46797E+01
   Friction velocity        uk    :  0.14664E-01 0.46758E+01
   Dimensionless distance   yplus :  0.99427E-02 0.29200E+01
   Friction thermal sca.    tstar :  0.12120E+01 0.17230E+03
   Rough dim-less th. sca.  tplus :  0.70434E-02 0.20686E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27683E+00      10   0.93164E-05   0.34194E+01 0.29737E+02 
c  Velocity[X]                                      0.13382E+01 
c  Velocity[Y]                                      0.90079E+00 
c  Velocity[Z]                                      0.11803E+01 
c  Pressure     0.12515E-04      16   0.24665E-03   0.12483E-01 0.10715E+02 
c  k            0.16256E-01      11   0.43531E-04   0.61755E-01 0.46600E+02 
c  omega        0.27922E+07       1   0.81380E-07   0.10823E+08 0.59188E+00 
c  TempK        0.10112E+05       5   0.40582E-05   0.89757E+01 0.10474E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6644e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.237          19.081        0.005057      -0.0087393
v  Velocity[Y]             -15.599          14.973         0.19288         0.28348
v  Velocity[Z]             -25.424          12.156         -1.6507        -0.50758
v  ǁVelocityǁ          0.0001651          25.599          7.7308          6.6973
v  Pressure                -517.08          202.29          25.491          29.239
v  k                   9.9012e-011          6.4968         0.19711          0.4163
v  omega                    57.482     2.7322e+008     1.2912e+006           76897
v  TempK                     298.5          363.17          336.19          343.75
v  TurbVisc            2.4812e-018       0.0012818     4.8477e-005      0.00017285
v  CourantNb           9.9402e-005          1.5005         0.79341         0.97534
v  FourierNb             0.0037761               1         0.40762         0.15364
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0033775     7.3503e-005      0.00019906

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.34          306.45
v  Yplus               0            2.92         0.63305         0.48992


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77205           2.094           1.201           1.129


 INSTANT    0.658000000E-02   TIME STEP NUMBER             658
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923993E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14647E-01 0.46797E+01
   Friction velocity        uk    :  0.14647E-01 0.46757E+01
   Dimensionless distance   yplus :  0.99311E-02 0.29200E+01
   Friction thermal sca.    tstar :  0.12119E+01 0.17250E+03
   Rough dim-less th. sca.  tplus :  0.70352E-02 0.20685E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27681E+00      10   0.93644E-05   0.34191E+01 0.29711E+02 
c  Velocity[X]                                      0.13371E+01 
c  Velocity[Y]                                      0.89720E+00 
c  Velocity[Z]                                      0.11848E+01 
c  Pressure     0.12238E-04      16   0.24636E-03   0.12207E-01 0.11639E+02 
c  k            0.16279E-01      11   0.44333E-04   0.62775E-01 0.46804E+02 
c  omega        0.27922E+07       1   0.81078E-07   0.97358E+07 0.57266E+00 
c  TempK        0.10113E+05       5   0.40478E-05   0.89339E+01 0.10452E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6637e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.237           19.08       0.0051212      -0.0087137
v  Velocity[Y]             -15.506          14.976          0.1933         0.28409
v  Velocity[Z]             -25.424          12.154         -1.6507         -0.5076
v  ǁVelocityǁ         0.00017598          25.599          7.7304          6.6967
v  Pressure                -516.93          202.32          25.529          29.284
v  k                   9.9007e-011          6.3893         0.19733         0.41682
v  omega                    57.482     2.7322e+008     1.2912e+006           76897
v  TempK                     298.5          363.17           336.2          343.77
v  TurbVisc            2.4811e-018       0.0012819     4.8535e-005      0.00017304
v  CourantNb            0.00011394          1.5007          0.7934         0.97533
v  FourierNb             0.0037764               1         0.40769         0.15378
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0033934      7.351e-005      0.00019909

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.34          306.45
v  Yplus               0            2.92         0.63303          0.4899


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78718          2.0942          1.2011          1.1291


 INSTANT    0.659000000E-02   TIME STEP NUMBER             659
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924031E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14641E-01 0.46796E+01
   Friction velocity        uk    :  0.14641E-01 0.46756E+01
   Dimensionless distance   yplus :  0.99269E-02 0.29200E+01
   Friction thermal sca.    tstar :  0.12119E+01 0.17258E+03
   Rough dim-less th. sca.  tplus :  0.70323E-02 0.20685E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27680E+00      10   0.94196E-05   0.34211E+01 0.29704E+02 
c  Velocity[X]                                      0.13359E+01 
c  Velocity[Y]                                      0.89544E+00 
c  Velocity[Z]                                      0.11898E+01 
c  Pressure     0.12299E-04      17   0.24808E-03   0.12268E-01 0.11539E+02 
c  k            0.16302E-01      11   0.44949E-04   0.63824E-01 0.47037E+02 
c  omega        0.27922E+07       1   0.79755E-07   0.62957E+07 0.50282E+00 
c  TempK        0.10113E+05       5   0.40375E-05   0.88931E+01 0.10430E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6627e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.236          19.079       0.0051861      -0.0086858
v  Velocity[Y]             -15.475          14.978         0.19372         0.28469
v  Velocity[Z]             -25.424          12.152         -1.6507        -0.50762
v  ǁVelocityǁ         0.00018545          25.599            7.73          6.6961
v  Pressure                -516.79          202.35          25.567          29.328
v  k                   9.9003e-011          6.4863         0.19756         0.41735
v  omega                    57.482     2.7322e+008     1.2912e+006           76897
v  TempK                     298.5          363.17          336.22          343.79
v  TurbVisc             2.481e-018       0.0012823     4.8594e-005      0.00017322
v  CourantNb            0.00013417          1.5009         0.79339         0.97531
v  FourierNb             0.0037767               1         0.40775         0.15392
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0034107     7.3516e-005      0.00019913

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.34          306.45
v  Yplus               0            2.92         0.63301         0.48987


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82379          2.0944          1.2011          1.1292


 INSTANT    0.660000000E-02   TIME STEP NUMBER             660
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924087E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14622E-01 0.46795E+01
   Friction velocity        uk    :  0.14622E-01 0.46755E+01
   Dimensionless distance   yplus :  0.99137E-02 0.29200E+01
   Friction thermal sca.    tstar :  0.12119E+01 0.17281E+03
   Rough dim-less th. sca.  tplus :  0.70229E-02 0.20685E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27679E+00      10   0.94862E-05   0.34256E+01 0.29718E+02 
c  Velocity[X]                                      0.13345E+01 
c  Velocity[Y]                                      0.89498E+00 
c  Velocity[Z]                                      0.11961E+01 
c  Pressure     0.12543E-04      18   0.25242E-03   0.12512E-01 0.12147E+02 
c  k            0.16325E-01      11   0.45563E-04   0.64829E-01 0.47277E+02 
c  omega        0.27922E+07       1   0.80627E-07   0.80663E+07 0.53782E+00 
c  TempK        0.10113E+05       5   0.40270E-05   0.88542E+01 0.10409E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6614e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.236          19.079       0.0052497      -0.0086569
v  Velocity[Y]             -15.499          14.981         0.19415          0.2853
v  Velocity[Z]             -25.424           12.15         -1.6507        -0.50763
v  ǁVelocityǁ         0.00019647          25.599          7.7296          6.6954
v  Pressure                -516.64          202.39          25.612          29.379
v  k                   9.8999e-011          6.6913         0.19779         0.41788
v  omega                    57.482     2.7322e+008     1.2912e+006           76897
v  TempK                     298.5          363.17          336.23          343.82
v  TurbVisc            2.4809e-018       0.0012831     4.8653e-005      0.00017341
v  CourantNb            0.00015664          1.5012         0.79337          0.9753
v  FourierNb              0.003777               1         0.40781         0.15407
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0034272     7.3523e-005      0.00019916

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.35          306.45
v  Yplus               0            2.92           0.633         0.48985


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82922          2.0947          1.2012          1.1294


 INSTANT    0.661000000E-02   TIME STEP NUMBER             661
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924239E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14599E-01 0.46794E+01
   Friction velocity        uk    :  0.14599E-01 0.46754E+01
   Dimensionless distance   yplus :  0.98983E-02 0.29199E+01
   Friction thermal sca.    tstar :  0.12120E+01 0.17308E+03
   Rough dim-less th. sca.  tplus :  0.70120E-02 0.20685E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27677E+00      10   0.95588E-05   0.34358E+01 0.29766E+02 
c  Velocity[X]                                      0.13348E+01 
c  Velocity[Y]                                      0.89754E+00 
c  Velocity[Z]                                      0.12035E+01 
c  Pressure     0.12883E-04      17   0.25755E-03   0.12851E-01 0.11972E+02 
c  k            0.16348E-01      11   0.46207E-04   0.65767E-01 0.47483E+02 
c  omega        0.27922E+07       1   0.83624E-07   0.13793E+08 0.64048E+00 
c  TempK        0.10114E+05       5   0.40168E-05   0.88147E+01 0.10388E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6597e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.236          19.078        0.005311      -0.0086269
v  Velocity[Y]             -15.573          14.984         0.19458          0.2859
v  Velocity[Z]             -25.424          12.147         -1.6507        -0.50764
v  ǁVelocityǁ         0.00020622          25.599          7.7292          6.6948
v  Pressure                -516.49          202.42          25.654          29.427
v  k                   9.8994e-011          6.7001         0.19802         0.41842
v  omega                    57.482     2.7322e+008     1.2912e+006           76897
v  TempK                    298.51          363.17          336.24          343.84
v  TurbVisc            2.4808e-018       0.0012843     4.8711e-005       0.0001736
v  CourantNb            0.00016052          1.5016         0.79335         0.97529
v  FourierNb             0.0037773               1         0.40787         0.15421
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0034415      7.353e-005      0.00019919

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.35          306.45
v  Yplus               0          2.9199         0.63298         0.48983


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77018          2.0952          1.2012          1.1295


 INSTANT    0.662000000E-02   TIME STEP NUMBER             662
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924073E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14571E-01 0.46793E+01
   Friction velocity        uk    :  0.14571E-01 0.46753E+01
   Dimensionless distance   yplus :  0.98796E-02 0.29199E+01
   Friction thermal sca.    tstar :  0.12123E+01 0.17340E+03
   Rough dim-less th. sca.  tplus :  0.69988E-02 0.20685E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27676E+00      10   0.96562E-05   0.34514E+01 0.29819E+02 
c  Velocity[X]                                      0.13357E+01 
c  Velocity[Y]                                      0.89900E+00 
c  Velocity[Z]                                      0.12168E+01 
c  Pressure     0.13136E-04      18   0.24973E-03   0.13104E-01 0.12917E+02 
c  k            0.16371E-01      11   0.46900E-04   0.66785E-01 0.47723E+02 
c  omega        0.27922E+07       1   0.83840E-07   0.13995E+08 0.63833E+00 
c  TempK        0.10114E+05       5   0.40065E-05   0.87756E+01 0.10366E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6578e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.235          19.077       0.0053744      -0.0085958
v  Velocity[Y]             -15.638          14.986         0.19501         0.28651
v  Velocity[Z]             -25.424          12.145         -1.6507        -0.50765
v  ǁVelocityǁ         0.00021695          25.598          7.7288          6.6941
v  Pressure                -516.32          202.47          25.706          29.486
v  k                    9.899e-011          6.5488         0.19825         0.41895
v  omega                    57.482     2.7322e+008     1.2912e+006           76897
v  TempK                    298.51          363.17          336.25          343.86
v  TurbVisc            2.4807e-018       0.0012863      4.877e-005      0.00017378
v  CourantNb            0.00016082           1.502         0.79334         0.97528
v  FourierNb             0.0037776               1         0.40794         0.15436
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0034497     7.3536e-005      0.00019923

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.35          306.45
v  Yplus               0          2.9199         0.63296         0.48981


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76316          2.0956          1.2013          1.1296


 INSTANT    0.663000000E-02   TIME STEP NUMBER             663
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924235E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14535E-01 0.46792E+01
   Friction velocity        uk    :  0.14535E-01 0.46752E+01
   Dimensionless distance   yplus :  0.98548E-02 0.29198E+01
   Friction thermal sca.    tstar :  0.12122E+01 0.17384E+03
   Rough dim-less th. sca.  tplus :  0.69812E-02 0.20684E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27674E+00      10   0.97521E-05   0.34599E+01 0.29864E+02 
c  Velocity[X]                                      0.13344E+01 
c  Velocity[Y]                                      0.90215E+00 
c  Velocity[Z]                                      0.12233E+01 
c  Pressure     0.13132E-04      18   0.24832E-03   0.13099E-01 0.11262E+02 
c  k            0.16394E-01      11   0.47681E-04   0.67928E-01 0.47990E+02 
c  omega        0.27922E+07       1   0.82991E-07   0.13995E+08 0.63791E+00 
c  TempK        0.10114E+05       5   0.39962E-05   0.87330E+01 0.10342E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6566e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.235          19.077       0.0054369      -0.0085634
v  Velocity[Y]             -15.605          14.989         0.19545         0.28711
v  Velocity[Z]             -25.424          12.142         -1.6507        -0.50766
v  ǁVelocityǁ         0.00022551          25.598          7.7284          6.6934
v  Pressure                -516.18           202.5           25.74          29.526
v  k                   9.8986e-011          6.3157         0.19848         0.41949
v  omega                    57.482     2.7322e+008     1.2912e+006           76897
v  TempK                    298.51          363.17          336.26          343.88
v  TurbVisc            2.4805e-018       0.0012892     4.8829e-005      0.00017397
v  CourantNb            0.00016117          1.5023         0.79332         0.97527
v  FourierNb             0.0037779               1           0.408          0.1545
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0034735     7.3543e-005      0.00019926

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.35          306.46
v  Yplus               0          2.9198         0.63294         0.48979


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.79545          2.0959          1.2013          1.1298


 INSTANT    0.664000000E-02   TIME STEP NUMBER             664
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924045E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14516E-01 0.46791E+01
   Friction velocity        uk    :  0.14516E-01 0.46751E+01
   Dimensionless distance   yplus :  0.98420E-02 0.29198E+01
   Friction thermal sca.    tstar :  0.12121E+01 0.17407E+03
   Rough dim-less th. sca.  tplus :  0.69721E-02 0.20684E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27673E+00      10   0.98329E-05   0.34555E+01 0.29805E+02 
c  Velocity[X]                                      0.13330E+01 
c  Velocity[Y]                                      0.89703E+00 
c  Velocity[Z]                                      0.12255E+01 
c  Pressure     0.12978E-04      18   0.24034E-03   0.12946E-01 0.12520E+02 
c  k            0.16418E-01      11   0.48623E-04   0.69061E-01 0.48244E+02 
c  omega        0.27922E+07       1   0.81063E-07   0.96533E+07 0.55101E+00 
c  TempK        0.10114E+05       5   0.39859E-05   0.86894E+01 0.10319E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6557e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.234          19.076       0.0054981      -0.0085287
v  Velocity[Y]             -15.512          14.992         0.19589         0.28771
v  Velocity[Z]             -25.424          12.139         -1.6507        -0.50767
v  ǁVelocityǁ         0.00023683          25.598           7.728          6.6927
v  Pressure                -516.03          202.54          25.787          29.581
v  k                   9.8982e-011          6.3198         0.19871         0.42004
v  omega                    57.482     2.7322e+008     1.2912e+006           76896
v  TempK                    298.51          363.17          336.28           343.9
v  TurbVisc            2.4804e-018        0.001293     4.8888e-005      0.00017416
v  CourantNb            0.00016141          1.5025         0.79331         0.97526
v  FourierNb             0.0037783               1         0.40806         0.15465
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0033942     7.3549e-005       0.0001993

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.35          306.46
v  Yplus               0          2.9198         0.63292         0.48977


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7447          2.0961          1.2014          1.1299


 INSTANT    0.665000000E-02   TIME STEP NUMBER             665
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924351E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14511E-01 0.46790E+01
   Friction velocity        uk    :  0.14511E-01 0.46750E+01
   Dimensionless distance   yplus :  0.98384E-02 0.29198E+01
   Friction thermal sca.    tstar :  0.12121E+01 0.17413E+03
   Rough dim-less th. sca.  tplus :  0.69696E-02 0.20684E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27671E+00      10   0.99062E-05   0.34522E+01 0.29763E+02 
c  Velocity[X]                                      0.13316E+01 
c  Velocity[Y]                                      0.89411E+00 
c  Velocity[Z]                                      0.12265E+01 
c  Pressure     0.12808E-04      17   0.23870E-03   0.12776E-01 0.11797E+02 
c  k            0.16442E-01      11   0.49420E-04   0.70275E-01 0.48539E+02 
c  omega        0.27922E+07       1   0.79212E-07   0.58335E+07 0.46530E+00 
c  TempK        0.10115E+05       5   0.39756E-05   0.86466E+01 0.10295E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6545e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.234          19.075       0.0055577      -0.0084921
v  Velocity[Y]             -15.481          14.995         0.19633         0.28831
v  Velocity[Z]             -25.424          12.137         -1.6507        -0.50768
v  ǁVelocityǁ         0.00024695          25.599          7.7276           6.692
v  Pressure                -515.88          202.57          25.828          29.628
v  k                   9.8977e-011          6.3248         0.19894         0.42059
v  omega                    57.482     2.7322e+008     1.2912e+006           76896
v  TempK                    298.51          363.17          336.29          343.92
v  TurbVisc            2.4803e-018       0.0012974     4.8948e-005      0.00017435
v  CourantNb             0.0001618          1.5027         0.79329         0.97524
v  FourierNb             0.0037786               1         0.40812          0.1548
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0033748     7.3555e-005      0.00019933

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.35          306.46
v  Yplus               0          2.9198          0.6329         0.48975


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48345          2.0964          1.2014            1.13


 INSTANT    0.666000000E-02   TIME STEP NUMBER             666
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924023E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14490E-01 0.46789E+01
   Friction velocity        uk    :  0.14490E-01 0.46749E+01
   Dimensionless distance   yplus :  0.98242E-02 0.29198E+01
   Friction thermal sca.    tstar :  0.12121E+01 0.17438E+03
   Rough dim-less th. sca.  tplus :  0.69595E-02 0.20684E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27670E+00      10   0.99958E-05   0.34530E+01 0.29742E+02 
c  Velocity[X]                                      0.13318E+01 
c  Velocity[Y]                                      0.89271E+00 
c  Velocity[Z]                                      0.12285E+01 
c  Pressure     0.12780E-04      18   0.23745E-03   0.12748E-01 0.13364E+02 
c  k            0.16466E-01      11   0.50279E-04   0.71563E-01 0.48858E+02 
c  omega        0.27922E+07       1   0.78927E-07   0.54977E+07 0.45379E+00 
c  TempK        0.10115E+05       5   0.39653E-05   0.86037E+01 0.10270E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6529e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.233          19.075       0.0056143      -0.0084543
v  Velocity[Y]             -15.504          14.998         0.19677          0.2889
v  Velocity[Z]             -25.425          12.134         -1.6507        -0.50769
v  ǁVelocityǁ         0.00025739          25.599          7.7271          6.6913
v  Pressure                -515.72          202.63          25.885          29.692
v  k                   9.8973e-011          6.4856         0.19917         0.42114
v  omega                    57.482     2.7322e+008     1.2912e+006           76896
v  TempK                    298.51          363.17           336.3          343.94
v  TurbVisc            2.4802e-018       0.0013025     4.9008e-005      0.00017454
v  CourantNb            0.00016212          1.5031         0.79328         0.97523
v  FourierNb              0.003779               1         0.40819         0.15495
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0033728     7.3562e-005      0.00019936

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.35          306.46
v  Yplus               0          2.9198         0.63289         0.48973


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63832          2.0967          1.2015          1.1302


 INSTANT    0.667000000E-02   TIME STEP NUMBER             667
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924220E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14470E-01 0.46788E+01
   Friction velocity        uk    :  0.14470E-01 0.46748E+01
   Dimensionless distance   yplus :  0.98107E-02 0.29197E+01
   Friction thermal sca.    tstar :  0.12121E+01 0.17462E+03
   Rough dim-less th. sca.  tplus :  0.69499E-02 0.20684E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27668E+00      10   0.10083E-04   0.34588E+01 0.29749E+02 
c  Velocity[X]                                      0.13321E+01 
c  Velocity[Y]                                      0.89218E+00 
c  Velocity[Z]                                      0.12345E+01 
c  Pressure     0.12906E-04      18   0.23905E-03   0.12874E-01 0.13212E+02 
c  k            0.16490E-01      11   0.50682E-04   0.72731E-01 0.49147E+02 
c  omega        0.27922E+07       1   0.81776E-07   0.11711E+08 0.57865E+00 
c  TempK        0.10115E+05       5   0.39550E-05   0.85621E+01 0.10246E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6509e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.232          19.074       0.0056675      -0.0084148
v  Velocity[Y]             -15.596          15.001         0.19721          0.2895
v  Velocity[Z]             -25.425          12.131         -1.6507        -0.50769
v  ǁVelocityǁ           0.000268          25.599          7.7267          6.6906
v  Pressure                -515.57          202.68          25.939          29.753
v  k                   9.8969e-011          6.6878         0.19941         0.42169
v  omega                    57.482     2.7322e+008     1.2912e+006           76896
v  TempK                    298.51          363.17          336.31          343.96
v  TurbVisc            2.4801e-018       0.0013079     4.9068e-005      0.00017473
v  CourantNb            0.00016246          1.5035         0.79326         0.97521
v  FourierNb             0.0037794               1         0.40825         0.15511
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0034842     7.3569e-005       0.0001994

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.36          306.46
v  Yplus               0          2.9197         0.63287          0.4897


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67169          2.0972          1.2015          1.1303


 INSTANT    0.668000000E-02   TIME STEP NUMBER             668
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924253E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14440E-01 0.46787E+01
   Friction velocity        uk    :  0.14439E-01 0.46747E+01
   Dimensionless distance   yplus :  0.97902E-02 0.29197E+01
   Friction thermal sca.    tstar :  0.12122E+01 0.17499E+03
   Rough dim-less th. sca.  tplus :  0.69355E-02 0.20684E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27666E+00      10   0.10166E-04   0.34712E+01 0.29808E+02 
c  Velocity[X]                                      0.13331E+01 
c  Velocity[Y]                                      0.89668E+00 
c  Velocity[Z]                                      0.12414E+01 
c  Pressure     0.13079E-04      18   0.24023E-03   0.13046E-01 0.14079E+02 
c  k            0.16515E-01      11   0.51249E-04   0.73902E-01 0.49444E+02 
c  omega        0.27922E+07       1   0.83260E-07   0.15560E+08 0.64208E+00 
c  TempK        0.10115E+05       5   0.39448E-05   0.85217E+01 0.10221E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6489e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.232          19.073       0.0057184       -0.008374
v  Velocity[Y]             -15.654          15.004         0.19766         0.29009
v  Velocity[Z]             -25.426          12.128         -1.6507        -0.50769
v  ǁVelocityǁ         0.00027933            25.6          7.7263          6.6899
v  Pressure                 -515.4          202.73          26.001          29.821
v  k                   9.8965e-011           6.579         0.19964         0.42225
v  omega                    57.482     2.7322e+008     1.2912e+006           76896
v  TempK                    298.51          363.17          336.32          343.98
v  TurbVisc              2.48e-018       0.0013136     4.9129e-005      0.00017493
v  CourantNb            0.00016281           1.504         0.79324         0.97519
v  FourierNb             0.0037797               1         0.40832         0.15527
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.003782     7.3575e-005      0.00019944

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.36          306.46
v  Yplus               0          2.9197         0.63285         0.48968


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7728          2.0977          1.2016          1.1305


 INSTANT    0.669000000E-02   TIME STEP NUMBER             669
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924307E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14409E-01 0.46785E+01
   Friction velocity        uk    :  0.14409E-01 0.46746E+01
   Dimensionless distance   yplus :  0.97693E-02 0.29197E+01
   Friction thermal sca.    tstar :  0.12125E+01 0.17536E+03
   Rough dim-less th. sca.  tplus :  0.69206E-02 0.20683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27665E+00      10   0.10250E-04   0.34824E+01 0.29839E+02 
c  Velocity[X]                                      0.13346E+01 
c  Velocity[Y]                                      0.89999E+00 
c  Velocity[Z]                                      0.12478E+01 
c  Pressure     0.13294E-04      18   0.24381E-03   0.13260E-01 0.13025E+02 
c  k            0.16540E-01      11   0.51911E-04   0.75126E-01 0.49743E+02 
c  omega        0.27922E+07       1   0.81429E-07   0.12049E+08 0.57757E+00 
c  TempK        0.10116E+05       5   0.39344E-05   0.84795E+01 0.10195E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6474e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.231          19.073       0.0057674      -0.0083302
v  Velocity[Y]             -15.582          15.007         0.19811         0.29068
v  Velocity[Z]             -25.426          12.125         -1.6506        -0.50769
v  ǁVelocityǁ         0.00029029            25.6          7.7259          6.6891
v  Pressure                -515.25          202.78          26.053           29.88
v  k                    9.896e-011          6.3534         0.19988         0.42281
v  omega                    57.482     2.7322e+008     1.2912e+006           76896
v  TempK                    298.52          363.17          336.34             344
v  TurbVisc            2.4799e-018       0.0013195     4.9189e-005      0.00017512
v  CourantNb             0.0001632          1.5043         0.79322         0.97518
v  FourierNb             0.0037801               1         0.40838         0.15542
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0037076     7.3582e-005      0.00019947

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.36          306.46
v  Yplus               0          2.9197         0.63283         0.48966


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72365           2.098          1.2016          1.1306


 INSTANT    0.670000000E-02   TIME STEP NUMBER             670
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924195E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14397E-01 0.46784E+01
   Friction velocity        uk    :  0.14397E-01 0.46745E+01
   Dimensionless distance   yplus :  0.97614E-02 0.29196E+01
   Friction thermal sca.    tstar :  0.12124E+01 0.17550E+03
   Rough dim-less th. sca.  tplus :  0.69150E-02 0.20683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27663E+00      10   0.10374E-04   0.34758E+01 0.29770E+02 
c  Velocity[X]                                      0.13335E+01 
c  Velocity[Y]                                      0.89493E+00 
c  Velocity[Z]                                      0.12473E+01 
c  Pressure     0.13022E-04      18   0.24330E-03   0.12989E-01 0.12676E+02 
c  k            0.16565E-01      11   0.52415E-04   0.76295E-01 0.50006E+02 
c  omega        0.27922E+07       1   0.79589E-07   0.88109E+07 0.50839E+00 
c  TempK        0.10116E+05       5   0.39240E-05   0.84394E+01 0.10170E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6461e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.23          19.072       0.0058135      -0.0082829
v  Velocity[Y]              -15.52           15.01         0.19856         0.29126
v  Velocity[Z]             -25.426          12.122         -1.6506        -0.50769
v  ǁVelocityǁ         0.00030162            25.6          7.7255          6.6884
v  Pressure                -515.11          202.83          26.103          29.937
v  k                   9.8956e-011          6.3628         0.20011         0.42337
v  omega                    57.481     2.7322e+008     1.2912e+006           76896
v  TempK                    298.52          363.17          336.35          344.02
v  TurbVisc            2.4798e-018       0.0013256      4.925e-005      0.00017532
v  CourantNb            0.00016356          1.5046         0.79321         0.97516
v  FourierNb             0.0037805               1         0.40844         0.15558
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0038917     7.3588e-005      0.00019951

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.36          306.46
v  Yplus               0          2.9196         0.63281         0.48963


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59201          2.0983          1.2017          1.1307


 INSTANT    0.671000000E-02   TIME STEP NUMBER             671
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924048E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14386E-01 0.46783E+01
   Friction velocity        uk    :  0.14386E-01 0.46743E+01
   Dimensionless distance   yplus :  0.97541E-02 0.29196E+01
   Friction thermal sca.    tstar :  0.12123E+01 0.17563E+03
   Rough dim-less th. sca.  tplus :  0.69099E-02 0.20683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27661E+00      10   0.10500E-04   0.34804E+01 0.29757E+02 
c  Velocity[X]                                      0.13346E+01 
c  Velocity[Y]                                      0.89342E+00 
c  Velocity[Z]                                      0.12524E+01 
c  Pressure     0.13182E-04      18   0.24544E-03   0.13149E-01 0.13997E+02 
c  k            0.16590E-01      11   0.52960E-04   0.77735E-01 0.50330E+02 
c  omega        0.27922E+07       1   0.77951E-07   0.52180E+07 0.42049E+00 
c  TempK        0.10116E+05       5   0.39137E-05   0.84004E+01 0.10145E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6446e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.229          19.071       0.0058548      -0.0082351
v  Velocity[Y]             -15.505          15.014         0.19901         0.29185
v  Velocity[Z]             -25.427          12.119         -1.6506        -0.50769
v  ǁVelocityǁ         0.00031331            25.6          7.7251          6.6876
v  Pressure                -514.96          202.88          26.164          30.005
v  k                   9.8952e-011          6.3732         0.20035         0.42394
v  omega                    57.481     2.7322e+008     1.2912e+006           76896
v  TempK                    298.52          363.17          336.36          344.04
v  TurbVisc            2.4797e-018       0.0013321     4.9311e-005      0.00017551
v  CourantNb            0.00016394           1.505         0.79319         0.97515
v  FourierNb             0.0037809               1         0.40851         0.15574
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0042808     7.3593e-005      0.00019954

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.36          306.46
v  Yplus               0          2.9196         0.63278         0.48961


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45943          2.0987          1.2017          1.1309


 INSTANT    0.672000000E-02   TIME STEP NUMBER             672
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924281E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14366E-01 0.46782E+01
   Friction velocity        uk    :  0.14366E-01 0.46742E+01
   Dimensionless distance   yplus :  0.97403E-02 0.29196E+01
   Friction thermal sca.    tstar :  0.12123E+01 0.17588E+03
   Rough dim-less th. sca.  tplus :  0.69001E-02 0.20683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27659E+00      10   0.10598E-04   0.34878E+01 0.29762E+02 
c  Velocity[X]                                      0.13359E+01 
c  Velocity[Y]                                      0.89275E+00 
c  Velocity[Z]                                      0.12591E+01 
c  Pressure     0.13303E-04      18   0.24686E-03   0.13269E-01 0.13254E+02 
c  k            0.16615E-01      11   0.53583E-04   0.79406E-01 0.50685E+02 
c  omega        0.27922E+07       1   0.77619E-07   0.49694E+07 0.41151E+00 
c  TempK        0.10116E+05       5   0.39033E-05   0.83594E+01 0.10119E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6427e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.228          19.071       0.0058928      -0.0081872
v  Velocity[Y]             -15.521          15.017         0.19947         0.29243
v  Velocity[Z]             -25.427          12.115         -1.6505        -0.50769
v  ǁVelocityǁ         0.00032518          25.601          7.7246          6.6869
v  Pressure                -514.82          202.94           26.22          30.068
v  k                   9.8947e-011          6.4701         0.20059          0.4245
v  omega                    57.481     2.7322e+008     1.2912e+006           76896
v  TempK                    298.52          363.17          336.37          344.06
v  TurbVisc            2.4796e-018       0.0013387     4.9373e-005      0.00017571
v  CourantNb            0.00016435          1.5054         0.79318         0.97514
v  FourierNb             0.0037813               1         0.40857          0.1559
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046934       7.36e-005      0.00019958

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.36          306.46
v  Yplus               0          2.9196         0.63276         0.48958


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42379          2.0991          1.2017           1.131


 INSTANT    0.673000000E-02   TIME STEP NUMBER             673
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924243E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14346E-01 0.46781E+01
   Friction velocity        uk    :  0.14346E-01 0.46741E+01
   Dimensionless distance   yplus :  0.97271E-02 0.29196E+01
   Friction thermal sca.    tstar :  0.12123E+01 0.17612E+03
   Rough dim-less th. sca.  tplus :  0.68908E-02 0.20683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27657E+00      10   0.10700E-04   0.34949E+01 0.29785E+02 
c  Velocity[X]                                      0.13359E+01 
c  Velocity[Y]                                      0.89246E+00 
c  Velocity[Z]                                      0.12665E+01 
c  Pressure     0.13443E-04      18   0.24756E-03   0.13409E-01 0.14020E+02 
c  k            0.16641E-01      11   0.54186E-04   0.81085E-01 0.51033E+02 
c  omega        0.27922E+07       1   0.79477E-07   0.83764E+07 0.49075E+00 
c  TempK        0.10116E+05       5   0.38930E-05   0.83188E+01 0.10094E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6404e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.228           19.07       0.0059301      -0.0081383
v  Velocity[Y]             -15.615          15.021         0.19992         0.29302
v  Velocity[Z]             -25.428          12.112         -1.6505        -0.50769
v  ǁVelocityǁ         0.00033631          25.602          7.7242          6.6861
v  Pressure                -514.66          202.99          26.281          30.135
v  k                   9.8943e-011          6.6112         0.20083         0.42507
v  omega                    57.481     2.7322e+008     1.2912e+006           76896
v  TempK                    298.52          363.17          336.38          344.08
v  TurbVisc            2.4795e-018       0.0013449     4.9435e-005      0.00017591
v  CourantNb            0.00016475          1.5059         0.79316         0.97512
v  FourierNb             0.0037817               1         0.40864         0.15606
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0049085     7.3606e-005      0.00019962

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.36          306.46
v  Yplus               0          2.9196         0.63274         0.48956


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54168          2.0996          1.2018          1.1312


 INSTANT    0.674000000E-02   TIME STEP NUMBER             674
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924205E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14312E-01 0.46779E+01
   Friction velocity        uk    :  0.14312E-01 0.46740E+01
   Dimensionless distance   yplus :  0.97039E-02 0.29196E+01
   Friction thermal sca.    tstar :  0.12123E+01 0.17655E+03
   Rough dim-less th. sca.  tplus :  0.68743E-02 0.20683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27655E+00      10   0.10799E-04   0.35054E+01 0.29828E+02 
c  Velocity[X]                                      0.13382E+01 
c  Velocity[Y]                                      0.89550E+00 
c  Velocity[Z]                                      0.12717E+01 
c  Pressure     0.13554E-04      17   0.25076E-03   0.13520E-01 0.14615E+02 
c  k            0.16667E-01      11   0.54792E-04   0.82948E-01 0.51418E+02 
c  omega        0.27922E+07       1   0.84080E-07   0.21077E+08 0.72011E+00 
c  TempK        0.10116E+05       5   0.38827E-05   0.82808E+01 0.10071E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6382e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.227          19.069       0.0059701      -0.0080869
v  Velocity[Y]             -15.657          15.024         0.20038          0.2936
v  Velocity[Z]             -25.429          12.109         -1.6505         -0.5077
v  ǁVelocityǁ         0.00034937          25.602          7.7238          6.6853
v  Pressure                -514.51          203.05          26.347          30.209
v  k                   9.8939e-011          6.4421         0.20106         0.42565
v  omega                    57.481     2.7322e+008     1.2912e+006           76896
v  TempK                    298.52          363.17          336.39           344.1
v  TurbVisc            2.4794e-018       0.0013509     4.9497e-005      0.00017611
v  CourantNb            0.00016512          1.5064         0.79314         0.97511
v  FourierNb             0.0037821               1          0.4087         0.15622
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.005038     7.3612e-005      0.00019965

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.36          306.47
v  Yplus               0          2.9196         0.63272         0.48953


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61928          2.1002          1.2018          1.1313


 INSTANT    0.675000000E-02   TIME STEP NUMBER             675
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924064E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14287E-01 0.46778E+01
   Friction velocity        uk    :  0.14287E-01 0.46738E+01
   Dimensionless distance   yplus :  0.96869E-02 0.29196E+01
   Friction thermal sca.    tstar :  0.12124E+01 0.17685E+03
   Rough dim-less th. sca.  tplus :  0.68623E-02 0.20683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27653E+00      10   0.10879E-04   0.35181E+01 0.29881E+02 
c  Velocity[X]                                      0.13400E+01 
c  Velocity[Y]                                      0.90021E+00 
c  Velocity[Z]                                      0.12779E+01 
c  Pressure     0.13876E-04      18   0.24846E-03   0.13841E-01 0.15086E+02 
c  k            0.16693E-01      11   0.56164E-04   0.84861E-01 0.51782E+02 
c  omega        0.27922E+07       1   0.81621E-07   0.13371E+08 0.59166E+00 
c  TempK        0.10116E+05       5   0.38724E-05   0.82430E+01 0.10046E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6365e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.226          19.069       0.0060084      -0.0080342
v  Velocity[Y]             -15.576          15.027         0.20085         0.29418
v  Velocity[Z]             -25.429          12.105         -1.6505         -0.5077
v  ǁVelocityǁ         0.00036107          25.603          7.7233          6.6845
v  Pressure                -514.35          203.12          26.416          30.285
v  k                   9.8934e-011          6.4244          0.2013         0.42622
v  omega                    57.481     2.7322e+008     1.2912e+006           76896
v  TempK                    298.52          363.17           336.4          344.12
v  TurbVisc            2.4793e-018       0.0013568     4.9559e-005      0.00017631
v  CourantNb            0.00016559          1.5068         0.79313         0.97509
v  FourierNb             0.0037825               1         0.40877         0.15638
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046545     7.3617e-005      0.00019968

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.37          306.47
v  Yplus               0          2.9196         0.63269          0.4895


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68989          2.1005          1.2019          1.1315


 INSTANT    0.676000000E-02   TIME STEP NUMBER             676
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924181E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14276E-01 0.46777E+01
   Friction velocity        uk    :  0.14276E-01 0.46737E+01
   Dimensionless distance   yplus :  0.96794E-02 0.29195E+01
   Friction thermal sca.    tstar :  0.12127E+01 0.17699E+03
   Rough dim-less th. sca.  tplus :  0.68570E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27651E+00      10   0.10963E-04   0.35251E+01 0.29865E+02 
c  Velocity[X]                                      0.13446E+01 
c  Velocity[Y]                                      0.89656E+00 
c  Velocity[Z]                                      0.12840E+01 
c  Pressure     0.13851E-04      17   0.24676E-03   0.13816E-01 0.14269E+02 
c  k            0.16719E-01      11   0.57412E-04   0.86774E-01 0.52164E+02 
c  omega        0.27922E+07       1   0.79447E-07   0.84327E+07 0.49281E+00 
c  TempK        0.10116E+05       5   0.38622E-05   0.82064E+01 0.10021E+01 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.635e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.225          19.068       0.0060464      -0.0079806
v  Velocity[Y]             -15.525          15.031         0.20132         0.29476
v  Velocity[Z]              -25.43          12.101         -1.6504         -0.5077
v  ǁVelocityǁ         0.00037454          25.603          7.7229          6.6837
v  Pressure                -514.21          203.18          26.479          30.355
v  k                    9.893e-011          6.4398         0.20155          0.4268
v  omega                    57.481     2.7322e+008     1.2912e+006           76896
v  TempK                    298.53          363.17          336.42          344.14
v  TurbVisc            2.4791e-018       0.0013625     4.9622e-005      0.00017652
v  CourantNb            0.00016598          1.5072         0.79311         0.97507
v  FourierNb             0.0037829               1         0.40883         0.15654
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0041408     7.3622e-005      0.00019971

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.37          306.47
v  Yplus               0          2.9195         0.63266         0.48947


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42334          2.1009          1.2019          1.1316


 INSTANT    0.677000000E-02   TIME STEP NUMBER             677
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924223E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14266E-01 0.46775E+01
   Friction velocity        uk    :  0.14266E-01 0.46736E+01
   Dimensionless distance   yplus :  0.96726E-02 0.29195E+01
   Friction thermal sca.    tstar :  0.12126E+01 0.17712E+03
   Rough dim-less th. sca.  tplus :  0.68521E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27649E+00      10   0.11011E-04   0.35453E+01 0.29873E+02 
c  Velocity[X]                                      0.13477E+01 
c  Velocity[Y]                                      0.89601E+00 
c  Velocity[Z]                                      0.13016E+01 
c  Pressure     0.14196E-04      18   0.24930E-03   0.14161E-01 0.13935E+02 
c  k            0.16745E-01      11   0.58590E-04   0.88862E-01 0.52611E+02 
c  omega        0.27922E+07       1   0.79259E-07   0.86514E+07 0.49935E+00 
c  TempK        0.10116E+05       5   0.38519E-05   0.81702E+01 0.99962E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6332e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.224          19.068       0.0060884      -0.0079229
v  Velocity[Y]              -15.52          15.035         0.20178         0.29535
v  Velocity[Z]             -25.431          12.098         -1.6504         -0.5077
v  ǁVelocityǁ         0.00038741          25.604          7.7224          6.6829
v  Pressure                -514.08          203.23          26.538          30.421
v  k                   9.8925e-011          6.4561         0.20179         0.42738
v  omega                    57.481     2.7322e+008     1.2912e+006           76896
v  TempK                    298.53          363.17          336.43          344.16
v  TurbVisc             2.479e-018       0.0013682     4.9685e-005      0.00017672
v  CourantNb            0.00016646          1.5076         0.79309         0.97506
v  FourierNb             0.0037833               1          0.4089          0.1567
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038194     7.3627e-005      0.00019975

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.37          306.47
v  Yplus               0          2.9195         0.63264         0.48945


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72294          2.1013           1.202          1.1318


 INSTANT    0.678000000E-02   TIME STEP NUMBER             678
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924212E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14244E-01 0.46774E+01
   Friction velocity        uk    :  0.14243E-01 0.46734E+01
   Dimensionless distance   yplus :  0.96573E-02 0.29195E+01
   Friction thermal sca.    tstar :  0.12125E+01 0.17740E+03
   Rough dim-less th. sca.  tplus :  0.68413E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27647E+00      10   0.11081E-04   0.35341E+01 0.29847E+02 
c  Velocity[X]                                      0.13491E+01 
c  Velocity[Y]                                      0.89532E+00 
c  Velocity[Z]                                      0.12897E+01 
c  Pressure     0.13927E-04      18   0.24853E-03   0.13893E-01 0.14671E+02 
c  k            0.16771E-01      11   0.59947E-04   0.91073E-01 0.53056E+02 
c  omega        0.27922E+07       1   0.77914E-07   0.53775E+07 0.42032E+00 
c  TempK        0.10116E+05       5   0.38417E-05   0.81343E+01 0.99721E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.631e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.222          19.067       0.0061292      -0.0078623
v  Velocity[Y]             -15.539          15.038         0.20226         0.29593
v  Velocity[Z]             -25.431          12.094         -1.6503        -0.50769
v  ǁVelocityǁ         0.00040018          25.604          7.7219           6.682
v  Pressure                -513.94          203.29          26.605          30.495
v  k                   9.8921e-011          6.4735         0.20203         0.42797
v  omega                    57.481     2.7322e+008     1.2912e+006           76895
v  TempK                    298.53          363.17          336.44          344.18
v  TurbVisc            2.4789e-018       0.0013739     4.9749e-005      0.00017693
v  CourantNb            0.00015125          1.5081         0.79308         0.97504
v  FourierNb             0.0037837               1         0.40896         0.15687
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038904     7.3634e-005      0.00019978

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.37          306.47
v  Yplus               0          2.9195         0.63261         0.48942


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63362          2.1018           1.202          1.1319


 INSTANT    0.679000000E-02   TIME STEP NUMBER             679
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924271E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14225E-01 0.46772E+01
   Friction velocity        uk    :  0.14225E-01 0.46733E+01
   Dimensionless distance   yplus :  0.96451E-02 0.29195E+01
   Friction thermal sca.    tstar :  0.12125E+01 0.17762E+03
   Rough dim-less th. sca.  tplus :  0.68326E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27645E+00      10   0.11151E-04   0.35460E+01 0.29876E+02 
c  Velocity[X]                                      0.13521E+01 
c  Velocity[Y]                                      0.89618E+00 
c  Velocity[Z]                                      0.12977E+01 
c  Pressure     0.14140E-04      18   0.24965E-03   0.14106E-01 0.15129E+02 
c  k            0.16798E-01      12   0.61369E-04   0.93492E-01 0.53518E+02 
c  omega        0.27922E+07       1   0.79702E-07   0.85050E+07 0.49383E+00 
c  TempK        0.10116E+05       5   0.38313E-05   0.80982E+01 0.99486E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6284e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.221          19.067        0.006169      -0.0078003
v  Velocity[Y]             -15.632          15.042         0.20273         0.29651
v  Velocity[Z]             -25.432           12.09         -1.6503        -0.50769
v  ǁVelocityǁ         0.00041297          25.605          7.7215          6.6812
v  Pressure                 -513.8          203.35          26.674          30.572
v  k                   9.8916e-011          6.4919         0.20228         0.42856
v  omega                    57.481     2.7322e+008     1.2912e+006           76895
v  TempK                    298.53          363.17          336.45           344.2
v  TurbVisc            2.4788e-018       0.0013797     4.9813e-005      0.00017714
v  CourantNb            0.00012492          1.5087         0.79306         0.97502
v  FourierNb             0.0037841               1         0.40903         0.15703
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038695      7.364e-005      0.00019982

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.37          306.47
v  Yplus               0          2.9195         0.63258         0.48939


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39964          2.1024          1.2021          1.1321


 INSTANT    0.680000000E-02   TIME STEP NUMBER             680
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924265E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14195E-01 0.46771E+01
   Friction velocity        uk    :  0.14195E-01 0.46731E+01
   Dimensionless distance   yplus :  0.96243E-02 0.29195E+01
   Friction thermal sca.    tstar :  0.12125E+01 0.17800E+03
   Rough dim-less th. sca.  tplus :  0.68179E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27643E+00      10   0.11862E-04   0.35540E+01 0.29917E+02 
c  Velocity[X]                                      0.13554E+01 
c  Velocity[Y]                                      0.89977E+00 
c  Velocity[Z]                                      0.12988E+01 
c  Pressure     0.13750E-04      18   0.25093E-03   0.13718E-01 0.15574E+02 
c  k            0.16824E-01      12   0.63585E-04   0.96059E-01 0.53990E+02 
c  omega        0.27922E+07       1   0.83577E-07   0.19388E+08 0.69684E+00 
c  TempK        0.10116E+05       5   0.38211E-05   0.80638E+01 0.99264E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6259e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.22          19.066       0.0062112      -0.0077398
v  Velocity[Y]              -15.67          15.046         0.20321         0.29709
v  Velocity[Z]             -25.433          12.086         -1.6503        -0.50768
v  ǁVelocityǁ         0.00042685          25.606           7.721          6.6803
v  Pressure                -513.65          203.42          26.748          30.653
v  k                   9.8912e-011          6.5113         0.20252         0.42915
v  omega                    57.481     2.7322e+008     1.2912e+006           76895
v  TempK                    298.53          363.17          336.46          344.22
v  TurbVisc            2.4787e-018       0.0013858     4.9877e-005      0.00017735
v  CourantNb            0.00011573          1.5092         0.79304         0.97501
v  FourierNb             0.0037846               1          0.4091         0.15721
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038587     7.3646e-005      0.00019985

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.37          306.47
v  Yplus               0          2.9195         0.63256         0.48936


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67332           2.103          1.2021          1.1322


 INSTANT    0.681000000E-02   TIME STEP NUMBER             681
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924287E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14172E-01 0.46770E+01
   Friction velocity        uk    :  0.14172E-01 0.46730E+01
   Dimensionless distance   yplus :  0.96092E-02 0.29195E+01
   Friction thermal sca.    tstar :  0.12125E+01 0.17829E+03
   Rough dim-less th. sca.  tplus :  0.68072E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27641E+00      10   0.11895E-04   0.35683E+01 0.29965E+02 
c  Velocity[X]                                      0.13596E+01 
c  Velocity[Y]                                      0.90396E+00 
c  Velocity[Z]                                      0.13047E+01 
c  Pressure     0.13726E-04      18   0.25761E-03   0.13696E-01 0.15578E+02 
c  k            0.16850E-01      12   0.66703E-04   0.99636E-01 0.54577E+02 
c  omega        0.27922E+07       1   0.81978E-07   0.14022E+08 0.60780E+00 
c  TempK        0.10116E+05       5   0.38109E-05   0.80280E+01 0.99032E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6239e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.219          19.065       0.0062482      -0.0076807
v  Velocity[Y]              -15.58           15.05         0.20369         0.29767
v  Velocity[Z]             -25.434          12.081         -1.6502        -0.50768
v  ǁVelocityǁ         0.00044076          25.607          7.7205          6.6795
v  Pressure                -513.52          203.49           26.82          30.733
v  k                   9.8907e-011          6.5317         0.20277         0.42975
v  omega                    57.481     2.7321e+008     1.2912e+006           76895
v  TempK                    298.53          363.17          336.47          344.24
v  TurbVisc            2.4786e-018       0.0013923     4.9942e-005      0.00017756
v  CourantNb            0.00013336          1.5097         0.79302         0.97499
v  FourierNb              0.003785               1         0.40917         0.15738
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038522     7.3653e-005      0.00019988

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.37          306.47
v  Yplus               0          2.9195         0.63253         0.48933


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56849          2.1035          1.2022          1.1324


 INSTANT    0.682000000E-02   TIME STEP NUMBER             682
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924229E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14163E-01 0.46768E+01
   Friction velocity        uk    :  0.14163E-01 0.46728E+01
   Dimensionless distance   yplus :  0.96029E-02 0.29195E+01
   Friction thermal sca.    tstar :  0.12127E+01 0.17840E+03
   Rough dim-less th. sca.  tplus :  0.68028E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27638E+00      10   0.12290E-04   0.35831E+01 0.29990E+02 
c  Velocity[X]                                      0.13680E+01 
c  Velocity[Y]                                      0.90463E+00 
c  Velocity[Z]                                      0.13104E+01 
c  Pressure     0.14712E-04      18   0.25433E-03   0.14681E-01 0.15994E+02 
c  k            0.16877E-01      12   0.70060E-04   0.10348E+00 0.55171E+02 
c  omega        0.27922E+07       1   0.80238E-07   0.95928E+07 0.52230E+00 
c  TempK        0.10116E+05       5   0.38010E-05   0.79923E+01 0.98811E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6219e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.217          19.065       0.0062854       -0.007623
v  Velocity[Y]             -15.519          15.054         0.20417         0.29826
v  Velocity[Z]             -25.435          12.077         -1.6502        -0.50768
v  ǁVelocityǁ         0.00045526          25.608          7.7201          6.6786
v  Pressure                -513.39          203.56          26.896          30.815
v  k                   9.8902e-011          6.5532         0.20302         0.43034
v  omega                    57.481     2.7321e+008     1.2912e+006           76895
v  TempK                    298.54          363.17          336.48          344.26
v  TurbVisc            2.4785e-018       0.0013992     5.0008e-005      0.00017778
v  CourantNb            0.00016407          1.5101           0.793         0.97497
v  FourierNb             0.0037854               1         0.40924         0.15755
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038084      7.366e-005      0.00019992

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.37          306.47
v  Yplus               0          2.9195          0.6325         0.48929


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63617          2.1039          1.2022          1.1325


 INSTANT    0.683000000E-02   TIME STEP NUMBER             683
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924235E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14157E-01 0.46767E+01
   Friction velocity        uk    :  0.14156E-01 0.46727E+01
   Dimensionless distance   yplus :  0.95983E-02 0.29195E+01
   Friction thermal sca.    tstar :  0.12129E+01 0.17849E+03
   Rough dim-less th. sca.  tplus :  0.67995E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27636E+00      10   0.12125E-04   0.35978E+01 0.30022E+02 
c  Velocity[X]                                      0.13757E+01 
c  Velocity[Y]                                      0.90434E+00 
c  Velocity[Z]                                      0.13178E+01 
c  Pressure     0.14367E-04      18   0.25507E-03   0.14337E-01 0.15462E+02 
c  k            0.16903E-01      12   0.73267E-04   0.10789E+00 0.55817E+02 
c  omega        0.27922E+07       1   0.80193E-07   0.90907E+07 0.51548E+00 
c  TempK        0.10116E+05       5   0.37909E-05   0.79576E+01 0.98587E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6196e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.216          19.064       0.0063208      -0.0075659
v  Velocity[Y]             -15.511          15.058         0.20466         0.29884
v  Velocity[Z]             -25.436          12.072         -1.6501        -0.50767
v  ǁVelocityǁ         0.00046881          25.608          7.7196          6.6777
v  Pressure                -513.27          203.62          26.968          30.895
v  k                   9.8898e-011          6.5757         0.20327         0.43094
v  omega                    57.481     2.7321e+008     1.2912e+006           76895
v  TempK                    298.54          363.17          336.49          344.28
v  TurbVisc            2.4784e-018       0.0014032     5.0074e-005      0.00017799
v  CourantNb            0.00016928          1.5107         0.79298         0.97494
v  FourierNb             0.0037858               1         0.40931         0.15773
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.003759     7.3667e-005      0.00019996

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.38          306.47
v  Yplus               0          2.9195         0.63247         0.48926


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4806          2.1045          1.2023          1.1327


 INSTANT    0.684000000E-02   TIME STEP NUMBER             684
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924257E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14139E-01 0.46765E+01
   Friction velocity        uk    :  0.14139E-01 0.46725E+01
   Dimensionless distance   yplus :  0.95865E-02 0.29195E+01
   Friction thermal sca.    tstar :  0.12128E+01 0.17871E+03
   Rough dim-less th. sca.  tplus :  0.67911E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27634E+00      10   0.12549E-04   0.36053E+01 0.30030E+02 
c  Velocity[X]                                      0.13808E+01 
c  Velocity[Y]                                      0.90449E+00 
c  Velocity[Z]                                      0.13200E+01 
c  Pressure     0.14048E-04      18   0.25591E-03   0.14019E-01 0.15479E+02 
c  k            0.16929E-01      12   0.75879E-04   0.11200E+00 0.56450E+02 
c  omega        0.27922E+07       1   0.78654E-07   0.55251E+07 0.43627E+00 
c  TempK        0.10116E+05       5   0.37810E-05   0.79243E+01 0.98373E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6169e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.215          19.064       0.0063584       -0.007511
v  Velocity[Y]             -15.532          15.062         0.20515         0.29943
v  Velocity[Z]             -25.437          12.068           -1.65        -0.50767
v  ǁVelocityǁ         0.00048369          25.609          7.7191          6.6768
v  Pressure                -513.15          203.69          27.039          30.975
v  k                   9.8893e-011          6.5992         0.20352         0.43154
v  omega                    57.481     2.7321e+008     1.2912e+006           76895
v  TempK                    298.54          363.17          336.51           344.3
v  TurbVisc            2.4782e-018       0.0014216      5.014e-005      0.00017821
v  CourantNb            0.00016974          1.5113         0.79296         0.97492
v  FourierNb             0.0037863               1         0.40938          0.1579
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.003715     7.3674e-005      0.00019999

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.38          306.47
v  Yplus               0          2.9195         0.63244         0.48922


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67316          2.1051          1.2023          1.1328


 INSTANT    0.685000000E-02   TIME STEP NUMBER             685
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924289E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14123E-01 0.46764E+01
   Friction velocity        uk    :  0.14122E-01 0.46724E+01
   Dimensionless distance   yplus :  0.95753E-02 0.29195E+01
   Friction thermal sca.    tstar :  0.12127E+01 0.17892E+03
   Rough dim-less th. sca.  tplus :  0.67832E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27631E+00      10   0.12443E-04   0.36168E+01 0.30074E+02 
c  Velocity[X]                                      0.13837E+01 
c  Velocity[Y]                                      0.90637E+00 
c  Velocity[Z]                                      0.13267E+01 
c  Pressure     0.14168E-04      18   0.25381E-03   0.14139E-01 0.16042E+02 
c  k            0.16956E-01      12   0.78678E-04   0.11610E+00 0.57086E+02 
c  omega        0.27922E+07       1   0.80399E-07   0.83995E+07 0.50439E+00 
c  TempK        0.10116E+05       5   0.37710E-05   0.78914E+01 0.98165E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6137e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.213          19.063       0.0063959      -0.0074537
v  Velocity[Y]               -15.6          15.066         0.20564         0.30001
v  Velocity[Z]             -25.438          12.063           -1.65        -0.50767
v  ǁVelocityǁ         0.00049771           25.61          7.7186          6.6759
v  Pressure                -513.03          203.76          27.115          31.058
v  k                   9.8888e-011          6.6237         0.20377         0.43214
v  omega                    57.481     2.7321e+008     1.2912e+006           76895
v  TempK                    298.54          363.17          336.52          344.32
v  TurbVisc            2.4781e-018       0.0014396     5.0207e-005      0.00017842
v  CourantNb            0.00017027           1.512         0.79294         0.97489
v  FourierNb             0.0037867               1         0.40945         0.15808
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036739     7.3681e-005      0.00020003

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.38          306.48
v  Yplus               0          2.9195         0.63241         0.48919


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4773          2.1058          1.2024           1.133


 INSTANT    0.686000000E-02   TIME STEP NUMBER             686
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924221E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14096E-01 0.46762E+01
   Friction velocity        uk    :  0.14096E-01 0.46722E+01
   Dimensionless distance   yplus :  0.95576E-02 0.29195E+01
   Friction thermal sca.    tstar :  0.12127E+01 0.17925E+03
   Rough dim-less th. sca.  tplus :  0.67706E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27629E+00      10   0.12239E-04   0.36303E+01 0.30133E+02 
c  Velocity[X]                                      0.13875E+01 
c  Velocity[Y]                                      0.91126E+00 
c  Velocity[Z]                                      0.13316E+01 
c  Pressure     0.13912E-04      18   0.25899E-03   0.13884E-01 0.16798E+02 
c  k            0.16982E-01      12   0.79445E-04   0.11893E+00 0.57590E+02 
c  omega        0.27922E+07       1   0.83276E-07   0.16465E+08 0.65812E+00 
c  TempK        0.10116E+05       5   0.37609E-05   0.78600E+01 0.97967E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6106e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.212          19.063        0.006438      -0.0073958
v  Velocity[Y]             -15.658           15.07         0.20612         0.30059
v  Velocity[Z]              -25.44          12.058         -1.6499        -0.50766
v  ǁVelocityǁ         0.00051305          25.612          7.7182           6.675
v  Pressure                 -512.9          203.83          27.197          31.148
v  k                   9.8884e-011          6.6491         0.20403         0.43275
v  omega                    57.481     2.7321e+008     1.2912e+006           76895
v  TempK                    298.54          363.17          336.53          344.34
v  TurbVisc             2.478e-018       0.0014561     5.0274e-005      0.00017864
v  CourantNb            0.00014936          1.5127         0.79292         0.97486
v  FourierNb             0.0037872               1         0.40952         0.15826
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036537     7.3688e-005      0.00020007

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.38          306.48
v  Yplus               0          2.9195         0.63239         0.48915


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71142          2.1065          1.2024          1.1331


 INSTANT    0.687000000E-02   TIME STEP NUMBER             687
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924265E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14074E-01 0.46761E+01
   Friction velocity        uk    :  0.14074E-01 0.46721E+01
   Dimensionless distance   yplus :  0.95427E-02 0.29195E+01
   Friction thermal sca.    tstar :  0.12127E+01 0.17953E+03
   Rough dim-less th. sca.  tplus :  0.67601E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27626E+00      10   0.12615E-04   0.36406E+01 0.30178E+02 
c  Velocity[X]                                      0.13917E+01 
c  Velocity[Y]                                      0.91707E+00 
c  Velocity[Z]                                      0.13319E+01 
c  Pressure     0.14108E-04      18   0.26506E-03   0.14081E-01 0.16682E+02 
c  k            0.17007E-01      12   0.79219E-04   0.12106E+00 0.57997E+02 
c  omega        0.27922E+07       1   0.80651E-07   0.92641E+07 0.52714E+00 
c  TempK        0.10116E+05       5   0.37510E-05   0.78287E+01 0.97758E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.608e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.21          19.062        0.006478      -0.0073403
v  Velocity[Y]             -15.592          15.074         0.20661         0.30117
v  Velocity[Z]             -25.441          12.054         -1.6499        -0.50766
v  ǁVelocityǁ         0.00052773          25.613          7.7177          6.6741
v  Pressure                -512.79           203.9          27.278          31.236
v  k                   9.8879e-011          6.6754         0.20429         0.43336
v  omega                     57.48     2.7321e+008     1.2912e+006           76895
v  TempK                    298.54          363.17          336.54          344.36
v  TurbVisc            2.4779e-018       0.0014702     5.0341e-005      0.00017886
v  CourantNb           7.8713e-005          1.5133         0.79289         0.97484
v  FourierNb             0.0037877               1         0.40959         0.15844
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036653     7.3696e-005      0.00020011

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.38          306.48
v  Yplus               0          2.9195         0.63236         0.48911


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48417          2.1071          1.2025          1.1333


 INSTANT    0.688000000E-02   TIME STEP NUMBER             688
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924240E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14065E-01 0.46759E+01
   Friction velocity        uk    :  0.14065E-01 0.46719E+01
   Dimensionless distance   yplus :  0.95361E-02 0.29196E+01
   Friction thermal sca.    tstar :  0.12127E+01 0.17965E+03
   Rough dim-less th. sca.  tplus :  0.67555E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27624E+00      10   0.12393E-04   0.36507E+01 0.30191E+02 
c  Velocity[X]                                      0.13960E+01 
c  Velocity[Y]                                      0.91594E+00 
c  Velocity[Z]                                      0.13387E+01 
c  Pressure     0.14278E-04      18   0.27411E-03   0.14252E-01 0.17240E+02 
c  k            0.17033E-01      12   0.79600E-04   0.12403E+00 0.58469E+02 
c  omega        0.27922E+07       1   0.80661E-07   0.84564E+07 0.50530E+00 
c  TempK        0.10116E+05       5   0.37411E-05   0.78013E+01 0.97572E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6056e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.209          19.062        0.006521      -0.0072855
v  Velocity[Y]             -15.551          15.079         0.20711         0.30176
v  Velocity[Z]             -25.442          12.051         -1.6498        -0.50765
v  ǁVelocityǁ         0.00054352          25.614          7.7172          6.6732
v  Pressure                -512.68          203.98          27.362          31.328
v  k                   9.8874e-011          6.7027         0.20454         0.43397
v  omega                     57.48     2.7321e+008     1.2912e+006           76895
v  TempK                    298.55          363.17          336.55          344.38
v  TurbVisc            2.4778e-018       0.0014824     5.0409e-005      0.00017908
v  CourantNb           1.3648e-005          1.5139         0.79287         0.97481
v  FourierNb             0.0037881               1         0.40966         0.15862
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037096     7.3704e-005      0.00020015

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.38          306.48
v  Yplus               0          2.9196         0.63233         0.48907


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6978          2.1077          1.2025          1.1334


 INSTANT    0.689000000E-02   TIME STEP NUMBER             689
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924210E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14058E-01 0.46758E+01
   Friction velocity        uk    :  0.14058E-01 0.46718E+01
   Dimensionless distance   yplus :  0.95314E-02 0.29196E+01
   Friction thermal sca.    tstar :  0.12131E+01 0.17974E+03
   Rough dim-less th. sca.  tplus :  0.67521E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27621E+00      10   0.12279E-04   0.36692E+01 0.30270E+02 
c  Velocity[X]                                      0.14033E+01 
c  Velocity[Y]                                      0.92323E+00 
c  Velocity[Z]                                      0.13426E+01 
c  Pressure     0.15067E-04      18   0.29113E-03   0.15042E-01 0.17971E+02 
c  k            0.17058E-01      12   0.79510E-04   0.12641E+00 0.58871E+02 
c  omega        0.27922E+07       1   0.82491E-07   0.14408E+08 0.62292E+00 
c  TempK        0.10115E+05       5   0.37314E-05   0.77723E+01 0.97385E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.6029e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.207          19.061       0.0065669      -0.0072325
v  Velocity[Y]             -15.556          15.083          0.2076         0.30234
v  Velocity[Z]             -25.443          12.048         -1.6497        -0.50765
v  ǁVelocityǁ         0.00055854          25.615          7.7167          6.6722
v  Pressure                -512.56          204.07          27.453          31.426
v  k                   9.8869e-011          6.7308         0.20481         0.43459
v  omega                     57.48     2.7321e+008     1.2912e+006           76894
v  TempK                    298.55          363.17          336.56           344.4
v  TurbVisc            2.4776e-018       0.0014931     5.0477e-005      0.00017931
v  CourantNb           4.7945e-005          1.5145         0.79285         0.97478
v  FourierNb             0.0037886               1         0.40973          0.1588
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037792     7.3711e-005      0.00020019

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.38          306.48
v  Yplus               0          2.9196         0.63229         0.48902


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49902          2.1083          1.2026          1.1336


 INSTANT    0.690000000E-02   TIME STEP NUMBER             690
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924347E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14044E-01 0.46756E+01
   Friction velocity        uk    :  0.14044E-01 0.46716E+01
   Dimensionless distance   yplus :  0.95221E-02 0.29196E+01
   Friction thermal sca.    tstar :  0.12132E+01 0.17992E+03
   Rough dim-less th. sca.  tplus :  0.67455E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27619E+00      10   0.12464E-04   0.36768E+01 0.30279E+02 
c  Velocity[X]                                      0.14081E+01 
c  Velocity[Y]                                      0.92467E+00 
c  Velocity[Z]                                      0.13440E+01 
c  Pressure     0.15109E-04      18   0.28868E-03   0.15085E-01 0.16366E+02 
c  k            0.17083E-01      12   0.80260E-04   0.12937E+00 0.59322E+02 
c  omega        0.27922E+07       1   0.80046E-07   0.73198E+07 0.47906E+00 
c  TempK        0.10115E+05       5   0.37218E-05   0.77422E+01 0.97181E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5999e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.206          19.061       0.0066124      -0.0071817
v  Velocity[Y]             -15.586          15.088          0.2081         0.30293
v  Velocity[Z]             -25.445          12.044         -1.6497        -0.50764
v  ǁVelocityǁ         0.00057491          25.616          7.7162          6.6713
v  Pressure                -512.47          204.14          27.531          31.512
v  k                   9.8865e-011          6.7597         0.20507         0.43521
v  omega                     57.48     2.7321e+008     1.2912e+006           76894
v  TempK                    298.55          363.17          336.57          344.41
v  TurbVisc            2.4775e-018       0.0015023     5.0547e-005      0.00017953
v  CourantNb            0.00010493          1.5152         0.79283         0.97476
v  FourierNb              0.003789               1         0.40981         0.15899
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038694     7.3719e-005      0.00020023

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.38          306.48
v  Yplus               0          2.9196         0.63226         0.48898


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69286           2.109          1.2026          1.1338


 INSTANT    0.691000000E-02   TIME STEP NUMBER             691
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924241E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14026E-01 0.46754E+01
   Friction velocity        uk    :  0.14026E-01 0.46715E+01
   Dimensionless distance   yplus :  0.95101E-02 0.29196E+01
   Friction thermal sca.    tstar :  0.12130E+01 0.18014E+03
   Rough dim-less th. sca.  tplus :  0.67370E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27616E+00      10   0.12342E-04   0.36909E+01 0.30319E+02 
c  Velocity[X]                                      0.14129E+01 
c  Velocity[Y]                                      0.92785E+00 
c  Velocity[Z]                                      0.13502E+01 
c  Pressure     0.15471E-04      17   0.28321E-03   0.15448E-01 0.17832E+02 
c  k            0.17108E-01      12   0.80886E-04   0.13221E+00 0.59761E+02 
c  omega        0.27922E+07       1   0.81138E-07   0.93186E+07 0.51904E+00 
c  TempK        0.10115E+05       5   0.37122E-05   0.77126E+01 0.96987E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5964e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.204           19.06       0.0066573      -0.0071332
v  Velocity[Y]             -15.686          15.092         0.20859         0.30351
v  Velocity[Z]             -25.446          12.041         -1.6496        -0.50763
v  ǁVelocityǁ            0.00059          25.617          7.7157          6.6703
v  Pressure                -512.36          204.22           27.62           31.61
v  k                    9.886e-011          6.7894         0.20533         0.43583
v  omega                     57.48     2.7321e+008     1.2912e+006           76894
v  TempK                    298.55          363.17          336.58          344.43
v  TurbVisc            2.4774e-018       0.0015108     5.0617e-005      0.00017976
v  CourantNb            0.00015699           1.516          0.7928         0.97474
v  FourierNb             0.0037895               1         0.40988         0.15919
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038727     7.3726e-005      0.00020027

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.38          306.48
v  Yplus               0          2.9196         0.63223         0.48893


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64578          2.1098          1.2027          1.1339


 INSTANT    0.692000000E-02   TIME STEP NUMBER             692
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924272E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14002E-01 0.46753E+01
   Friction velocity        uk    :  0.14002E-01 0.46713E+01
   Dimensionless distance   yplus :  0.94936E-02 0.29196E+01
   Friction thermal sca.    tstar :  0.12130E+01 0.18046E+03
   Rough dim-less th. sca.  tplus :  0.67254E-02 0.20683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27614E+00      10   0.13059E-04   0.37033E+01 0.30380E+02 
c  Velocity[X]                                      0.14174E+01 
c  Velocity[Y]                                      0.93465E+00 
c  Velocity[Z]                                      0.13513E+01 
c  Pressure     0.15124E-04      18   0.27831E-03   0.15102E-01 0.17235E+02 
c  k            0.17133E-01      12   0.81798E-04   0.13516E+00 0.60199E+02 
c  omega        0.27922E+07       1   0.85285E-07   0.20383E+08 0.71465E+00 
c  TempK        0.10115E+05       5   0.37034E-05   0.76855E+01 0.96803E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5931e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.202           19.06       0.0067041      -0.0070877
v  Velocity[Y]             -15.737          15.096         0.20908          0.3041
v  Velocity[Z]             -25.447          12.038         -1.6495        -0.50763
v  ǁVelocityǁ         0.00060617          25.619          7.7152          6.6694
v  Pressure                -512.26           204.3          27.705          31.702
v  k                   9.8855e-011          6.8196          0.2056         0.43646
v  omega                     57.48     2.7321e+008     1.2912e+006           76894
v  TempK                    298.55          363.17          336.59          344.45
v  TurbVisc            2.4773e-018       0.0015192     5.0687e-005      0.00017999
v  CourantNb            0.00017397          1.5167         0.79278         0.97471
v  FourierNb             0.0037899               1         0.40996         0.15938
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038765     7.3734e-005      0.00020031

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.38          306.48
v  Yplus               0          2.9196          0.6322         0.48889


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58526          2.1106          1.2027          1.1341


 INSTANT    0.693000000E-02   TIME STEP NUMBER             693
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924257E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13980E-01 0.46751E+01
   Friction velocity        uk    :  0.13980E-01 0.46712E+01
   Dimensionless distance   yplus :  0.94784E-02 0.29196E+01
   Friction thermal sca.    tstar :  0.12130E+01 0.18075E+03
   Rough dim-less th. sca.  tplus :  0.67146E-02 0.20683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27611E+00      10   0.12770E-04   0.37191E+01 0.30431E+02 
c  Velocity[X]                                      0.14222E+01 
c  Velocity[Y]                                      0.94212E+00 
c  Velocity[Z]                                      0.13548E+01 
c  Pressure     0.15356E-04      18   0.27399E-03   0.15336E-01 0.17556E+02 
c  k            0.17158E-01      12   0.83707E-04   0.13857E+00 0.60689E+02 
c  omega        0.27922E+07       1   0.80926E-07   0.91066E+07 0.51379E+00 
c  TempK        0.10115E+05       5   0.36947E-05   0.76581E+01 0.96607E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5904e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.201           19.06       0.0067475      -0.0070441
v  Velocity[Y]             -15.663            15.1         0.20958         0.30468
v  Velocity[Z]             -25.449          12.034         -1.6494        -0.50763
v  ǁVelocityǁ         0.00062188           25.62          7.7147          6.6684
v  Pressure                -512.17          204.38          27.792          31.798
v  k                    9.885e-011          6.8499         0.20587         0.43709
v  omega                     57.48     2.7321e+008     1.2912e+006           76894
v  TempK                    298.55          363.17           336.6          344.47
v  TurbVisc            2.4772e-018       0.0015275     5.0758e-005      0.00018021
v  CourantNb            0.00017453          1.5173         0.79276         0.97469
v  FourierNb             0.0037904               1         0.41004         0.15958
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038808     7.3743e-005      0.00020036

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.39          306.48
v  Yplus               0          2.9196         0.63217         0.48884


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63723          2.1112          1.2028          1.1343


 INSTANT    0.694000000E-02   TIME STEP NUMBER             694
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924233E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13973E-01 0.46750E+01
   Friction velocity        uk    :  0.13972E-01 0.46710E+01
   Dimensionless distance   yplus :  0.94736E-02 0.29196E+01
   Friction thermal sca.    tstar :  0.12130E+01 0.18084E+03
   Rough dim-less th. sca.  tplus :  0.67111E-02 0.20683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27608E+00      10   0.12148E-04   0.37341E+01 0.30439E+02 
c  Velocity[X]                                      0.14278E+01 
c  Velocity[Y]                                      0.94330E+00 
c  Velocity[Z]                                      0.13629E+01 
c  Pressure     0.14840E-04      18   0.26994E-03   0.14821E-01 0.17299E+02 
c  k            0.17182E-01      12   0.85297E-04   0.14160E+00 0.61130E+02 
c  omega        0.27922E+07       1   0.80168E-07   0.69185E+07 0.46180E+00 
c  TempK        0.10114E+05       5   0.36869E-05   0.76335E+01 0.96428E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.588e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.199          19.059       0.0067941      -0.0070007
v  Velocity[Y]             -15.622          15.105         0.21008         0.30527
v  Velocity[Z]              -25.45           12.03         -1.6493        -0.50762
v  ǁVelocityǁ         0.00063825          25.621          7.7142          6.6674
v  Pressure                -512.09          204.45          27.877          31.891
v  k                   9.8845e-011          6.8793         0.20614         0.43772
v  omega                     57.48     2.7321e+008     1.2912e+006           76894
v  TempK                    298.55          363.17          336.61          344.49
v  TurbVisc             2.477e-018        0.001536     5.0829e-005      0.00018044
v  CourantNb            0.00017507          1.5179         0.79273         0.97467
v  FourierNb             0.0037908               1         0.41012         0.15978
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038858      7.375e-005       0.0002004

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.39          306.48
v  Yplus               0          2.9196         0.63213          0.4888


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70695          2.1118          1.2028          1.1344


 INSTANT    0.695000000E-02   TIME STEP NUMBER             695
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924194E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13965E-01 0.46748E+01
   Friction velocity        uk    :  0.13965E-01 0.46709E+01
   Dimensionless distance   yplus :  0.94685E-02 0.29197E+01
   Friction thermal sca.    tstar :  0.12131E+01 0.18094E+03
   Rough dim-less th. sca.  tplus :  0.67075E-02 0.20683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27606E+00      10   0.14336E-04   0.37468E+01 0.30505E+02 
c  Velocity[X]                                      0.14344E+01 
c  Velocity[Y]                                      0.94991E+00 
c  Velocity[Z]                                      0.13625E+01 
c  Pressure     0.14884E-04      18   0.26741E-03   0.14868E-01 0.18458E+02 
c  k            0.17207E-01      12   0.85656E-04   0.14375E+00 0.61482E+02 
c  omega        0.27922E+07       1   0.81878E-07   0.98546E+07 0.52802E+00 
c  TempK        0.10114E+05       5   0.36788E-05   0.76102E+01 0.96259E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5854e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.197          19.059       0.0068417      -0.0069577
v  Velocity[Y]             -15.626          15.109         0.21058         0.30585
v  Velocity[Z]             -25.452          12.026         -1.6493        -0.50762
v  ǁVelocityǁ         0.00065482          25.622          7.7137          6.6664
v  Pressure                -512.01          204.54          27.971          31.993
v  k                   9.8841e-011          6.9075         0.20641         0.43835
v  omega                     57.48     2.7321e+008     1.2912e+006           76894
v  TempK                    298.55          363.17          336.63          344.51
v  TurbVisc            2.4769e-018       0.0015438     5.0901e-005      0.00018067
v  CourantNb            0.00017563          1.5185         0.79271         0.97465
v  FourierNb             0.0037914               1         0.41019         0.15997
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0040658     7.3757e-005      0.00020044

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.39          306.48
v  Yplus               0          2.9197          0.6321         0.48875


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54807          2.1124          1.2029          1.1346


 INSTANT    0.696000000E-02   TIME STEP NUMBER             696
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924373E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13951E-01 0.46747E+01
   Friction velocity        uk    :  0.13951E-01 0.46707E+01
   Dimensionless distance   yplus :  0.94591E-02 0.29197E+01
   Friction thermal sca.    tstar :  0.12135E+01 0.18112E+03
   Rough dim-less th. sca.  tplus :  0.67009E-02 0.20683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27603E+00      10   0.14307E-04   0.37701E+01 0.30588E+02 
c  Velocity[X]                                      0.14425E+01 
c  Velocity[Y]                                      0.95842E+00 
c  Velocity[Z]                                      0.13692E+01 
c  Pressure     0.15221E-04      18   0.26859E-03   0.15206E-01 0.16669E+02 
c  k            0.17231E-01      12   0.85600E-04   0.14627E+00 0.61858E+02 
c  omega        0.27922E+07       1   0.82664E-07   0.11459E+08 0.56193E+00 
c  TempK        0.10114E+05       5   0.36713E-05   0.75849E+01 0.96074E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5824e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.196          19.059       0.0068895      -0.0069155
v  Velocity[Y]              -15.69          15.114         0.21108         0.30644
v  Velocity[Z]             -25.453          12.023         -1.6492        -0.50761
v  ǁVelocityǁ         0.00067111          25.624          7.7132          6.6654
v  Pressure                -511.94          204.61          28.052          32.081
v  k                   9.8836e-011          6.9339         0.20669         0.43898
v  omega                     57.48     2.7321e+008     1.2912e+006           76894
v  TempK                    298.55          363.17          336.64          344.53
v  TurbVisc            2.4768e-018       0.0015293     5.0974e-005      0.00018091
v  CourantNb            0.00017621          1.5192         0.79269         0.97462
v  FourierNb             0.0037919               1         0.41027         0.16017
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0042241     7.3763e-005      0.00020048

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.39          306.48
v  Yplus               0          2.9197         0.63207          0.4887


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52407          2.1131           1.203          1.1348


 INSTANT    0.697000000E-02   TIME STEP NUMBER             697
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924157E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13930E-01 0.46745E+01
   Friction velocity        uk    :  0.13930E-01 0.46706E+01
   Dimensionless distance   yplus :  0.94450E-02 0.29197E+01
   Friction thermal sca.    tstar :  0.12134E+01 0.18139E+03
   Rough dim-less th. sca.  tplus :  0.66909E-02 0.20683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27600E+00      10   0.12278E-04   0.37919E+01 0.30639E+02 
c  Velocity[X]                                      0.14503E+01 
c  Velocity[Y]                                      0.96432E+00 
c  Velocity[Z]                                      0.13774E+01 
c  Pressure     0.15121E-04      18   0.26585E-03   0.15110E-01 0.17918E+02 
c  k            0.17256E-01      12   0.86122E-04   0.14896E+00 0.62217E+02 
c  omega        0.27922E+07       1   0.84659E-07   0.15187E+08 0.62996E+00 
c  TempK        0.10114E+05       5   0.36621E-05   0.75631E+01 0.95903E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5793e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.194          19.058       0.0069393      -0.0068731
v  Velocity[Y]             -15.765          15.118         0.21158         0.30702
v  Velocity[Z]             -25.454          12.019         -1.6491         -0.5076
v  ǁVelocityǁ         0.00067149          25.625          7.7127          6.6644
v  Pressure                -511.86           204.7          28.142          32.179
v  k                   9.8831e-011          6.9586         0.20696         0.43962
v  omega                     57.48     2.7321e+008     1.2912e+006           76893
v  TempK                    298.55          363.17          336.65          344.54
v  TurbVisc            2.4767e-018       0.0015066     5.1046e-005      0.00018115
v  CourantNb            0.00017677          1.5199         0.79266         0.97459
v  FourierNb             0.0037925               1         0.41035         0.16037
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0046466      7.377e-005      0.00020052

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.39          306.49
v  Yplus               0          2.9197         0.63203         0.48865


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5717          2.1138           1.203           1.135


 INSTANT    0.698000000E-02   TIME STEP NUMBER             698
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924342E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13905E-01 0.46744E+01
   Friction velocity        uk    :  0.13905E-01 0.46704E+01
   Dimensionless distance   yplus :  0.94276E-02 0.29197E+01
   Friction thermal sca.    tstar :  0.12133E+01 0.18172E+03
   Rough dim-less th. sca.  tplus :  0.66786E-02 0.20683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27597E+00      10   0.12328E-04   0.38071E+01 0.30711E+02 
c  Velocity[X]                                      0.14574E+01 
c  Velocity[Y]                                      0.97389E+00 
c  Velocity[Z]                                      0.13758E+01 
c  Pressure     0.14874E-04      18   0.26672E-03   0.14865E-01 0.16533E+02 
c  k            0.17280E-01      12   0.86583E-04   0.15050E+00 0.62466E+02 
c  omega        0.27922E+07       1   0.82089E-07   0.10538E+08 0.54429E+00 
c  TempK        0.10113E+05       5   0.36539E-05   0.75418E+01 0.95729E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.577e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.192          19.058       0.0069858      -0.0068314
v  Velocity[Y]             -15.735          15.122         0.21208         0.30761
v  Velocity[Z]             -25.456          12.014          -1.649        -0.50759
v  ǁVelocityǁ          0.0006703          25.626          7.7122          6.6634
v  Pressure                 -511.8          204.77          28.222          32.267
v  k                   9.8826e-011          6.9814         0.20724         0.44025
v  omega                     57.48     2.7321e+008     1.2912e+006           76893
v  TempK                    298.55          363.17          336.66          344.56
v  TurbVisc            2.4766e-018       0.0014856     5.1119e-005      0.00018138
v  CourantNb            0.00017731          1.5205         0.79264         0.97456
v  FourierNb             0.0037931               1         0.41042         0.16057
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0051112     7.3777e-005      0.00020057

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.39          306.49
v  Yplus               0          2.9197           0.632          0.4886


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52946          2.1144          1.2031          1.1351


 INSTANT    0.699000000E-02   TIME STEP NUMBER             699
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924334E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13891E-01 0.46742E+01
   Friction velocity        uk    :  0.13891E-01 0.46703E+01
   Dimensionless distance   yplus :  0.94183E-02 0.29197E+01
   Friction thermal sca.    tstar :  0.12133E+01 0.18190E+03
   Rough dim-less th. sca.  tplus :  0.66720E-02 0.20683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27594E+00      10   0.13143E-04   0.38220E+01 0.30731E+02 
c  Velocity[X]                                      0.14642E+01 
c  Velocity[Y]                                      0.97811E+00 
c  Velocity[Z]                                      0.13797E+01 
c  Pressure     0.15016E-04      18   0.26513E-03   0.15009E-01 0.16294E+02 
c  k            0.17305E-01      12   0.87740E-04   0.15264E+00 0.62755E+02 
c  omega        0.27922E+07       1   0.81255E-07   0.83910E+07 0.49865E+00 
c  TempK        0.10113E+05       5   0.36462E-05   0.75222E+01 0.95566E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.575e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.191          19.058       0.0070332      -0.0067906
v  Velocity[Y]             -15.643          15.126         0.21259          0.3082
v  Velocity[Z]             -25.457           12.01         -1.6489        -0.50758
v  ǁVelocityǁ         0.00065632          25.627          7.7116          6.6623
v  Pressure                -511.76          204.84          28.299          32.353
v  k                   9.8821e-011          7.0023         0.20751          0.4409
v  omega                     57.48     2.7321e+008     1.2912e+006           76893
v  TempK                    298.55          363.17          336.67          344.58
v  TurbVisc            2.4764e-018       0.0014661     5.1192e-005      0.00018161
v  CourantNb             0.0001779          1.5209         0.79261         0.97453
v  FourierNb             0.0037937               1          0.4105         0.16077
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0056223     7.3784e-005      0.00020061

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.39          306.49
v  Yplus               0          2.9197         0.63196         0.48855


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6375          2.1148          1.2031          1.1353


 INSTANT    0.700000000E-02   TIME STEP NUMBER             700
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924200E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13889E-01 0.46741E+01
   Friction velocity        uk    :  0.13889E-01 0.46701E+01
   Dimensionless distance   yplus :  0.94169E-02 0.29197E+01
   Friction thermal sca.    tstar :  0.12133E+01 0.18193E+03
   Rough dim-less th. sca.  tplus :  0.66710E-02 0.20684E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27592E+00      10   0.13781E-04   0.38409E+01 0.30774E+02 
c  Velocity[X]                                      0.14711E+01 
c  Velocity[Y]                                      0.98422E+00 
c  Velocity[Z]                                      0.13856E+01 
c  Pressure     0.14946E-04      18   0.26440E-03   0.14942E-01 0.17543E+02 
c  k            0.17330E-01      12   0.89980E-04   0.15570E+00 0.63123E+02 
c  omega        0.27922E+07       1   0.79976E-07   0.54717E+07 0.42805E+00 
c  TempK        0.10113E+05       5   0.36386E-05   0.75073E+01 0.95421E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5727e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.189          19.058       0.0070777      -0.0067501
v  Velocity[Y]             -15.616          15.131          0.2131         0.30878
v  Velocity[Z]             -25.459          12.006         -1.6489        -0.50757
v  ǁVelocityǁ         0.00064238          25.629          7.7111          6.6613
v  Pressure                -511.71          204.93          28.387          32.449
v  k                   9.8816e-011          7.0215         0.20779         0.44154
v  omega                     57.48     2.7321e+008     1.2912e+006           76893
v  TempK                    298.55          363.17          336.68           344.6
v  TurbVisc            2.4763e-018       0.0014961     5.1267e-005      0.00018185
v  CourantNb            0.00017849          1.5214         0.79259          0.9745
v  FourierNb             0.0037943               1         0.41058         0.16097
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0061788      7.379e-005      0.00020065

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.39          306.49
v  Yplus               0          2.9197         0.63193          0.4885


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73628          2.1154          1.2032          1.1355


 INSTANT    0.701000000E-02   TIME STEP NUMBER             701
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924327E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13880E-01 0.46739E+01
   Friction velocity        uk    :  0.13880E-01 0.46700E+01
   Dimensionless distance   yplus :  0.94106E-02 0.29198E+01
   Friction thermal sca.    tstar :  0.12133E+01 0.18205E+03
   Rough dim-less th. sca.  tplus :  0.66665E-02 0.20684E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27589E+00      10   0.13477E-04   0.38590E+01 0.30831E+02 
c  Velocity[X]                                      0.14789E+01 
c  Velocity[Y]                                      0.99173E+00 
c  Velocity[Z]                                      0.13883E+01 
c  Pressure     0.15076E-04      18   0.26846E-03   0.15075E-01 0.16698E+02 
c  k            0.17355E-01      12   0.91792E-04   0.15961E+00 0.63564E+02 
c  omega        0.27922E+07       1   0.79862E-07   0.50677E+07 0.41775E+00 
c  TempK        0.10112E+05       5   0.36309E-05   0.74926E+01 0.95290E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5702e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.187          19.058       0.0071199        -0.00671
v  Velocity[Y]             -15.643          15.135         0.21361         0.30937
v  Velocity[Z]              -25.46          12.001         -1.6488        -0.50757
v  ǁVelocityǁ         0.00062857          25.631          7.7106          6.6603
v  Pressure                -511.68             205          28.468          32.539
v  k                   9.8811e-011          7.0391         0.20806         0.44218
v  omega                     57.48     2.7321e+008     1.2912e+006           76893
v  TempK                    298.55          363.17          336.69          344.62
v  TurbVisc            2.4762e-018       0.0015287     5.1341e-005      0.00018208
v  CourantNb            0.00017908           1.522         0.79256         0.97447
v  FourierNb              0.003795               1         0.41065         0.16116
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0040326     7.3794e-005      0.00020068

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.39          306.49
v  Yplus               0          2.9198          0.6319         0.48845


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61585           2.116          1.2032          1.1356


 INSTANT    0.702000000E-02   TIME STEP NUMBER             702
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924160E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13863E-01 0.46738E+01
   Friction velocity        uk    :  0.13863E-01 0.46698E+01
   Dimensionless distance   yplus :  0.93995E-02 0.29198E+01
   Friction thermal sca.    tstar :  0.12133E+01 0.18227E+03
   Rough dim-less th. sca.  tplus :  0.66587E-02 0.20684E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27586E+00      10   0.13455E-04   0.38896E+01 0.30929E+02 
c  Velocity[X]                                      0.14878E+01 
c  Velocity[Y]                                      0.10011E+01 
c  Velocity[Z]                                      0.14006E+01 
c  Pressure     0.15232E-04      18   0.26962E-03   0.15233E-01 0.18297E+02 
c  k            0.17381E-01      12   0.93206E-04   0.16295E+00 0.63967E+02 
c  omega        0.27922E+07       1   0.84607E-07   0.13929E+08 0.59906E+00 
c  TempK        0.10112E+05       5   0.36224E-05   0.74787E+01 0.95178E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5673e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.185          19.058       0.0071612      -0.0066702
v  Velocity[Y]             -15.752           15.14         0.21412         0.30996
v  Velocity[Z]             -25.462          11.996         -1.6487        -0.50756
v  ǁVelocityǁ         0.00061484          25.632          7.7101          6.6593
v  Pressure                -511.63          205.09          28.561          32.639
v  k                   9.8806e-011          7.0552         0.20834         0.44283
v  omega                     57.48     2.7321e+008     1.2912e+006           76893
v  TempK                    298.55          363.17           336.7          344.63
v  TurbVisc            2.4761e-018       0.0015595     5.1415e-005      0.00018232
v  CourantNb            0.00017967          1.5227         0.79254         0.97444
v  FourierNb             0.0037956               1         0.41073         0.16136
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038825     7.3799e-005      0.00020071

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.39          306.49
v  Yplus               0          2.9198         0.63187          0.4884


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85031          2.1166          1.2033          1.1358


 INSTANT    0.703000000E-02   TIME STEP NUMBER             703
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924213E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13846E-01 0.46736E+01
   Friction velocity        uk    :  0.13846E-01 0.46697E+01
   Dimensionless distance   yplus :  0.93877E-02 0.29199E+01
   Friction thermal sca.    tstar :  0.12137E+01 0.18250E+03
   Rough dim-less th. sca.  tplus :  0.66503E-02 0.20684E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27583E+00      10   0.12764E-04   0.39100E+01 0.31049E+02 
c  Velocity[X]                                      0.14977E+01 
c  Velocity[Y]                                      0.10163E+01 
c  Velocity[Z]                                      0.13960E+01 
c  Pressure     0.15339E-04      18   0.27503E-03   0.15343E-01 0.17930E+02 
c  k            0.17407E-01      12   0.93373E-04   0.16713E+00 0.64407E+02 
c  omega        0.27922E+07       1   0.86135E-07   0.20071E+08 0.70709E+00 
c  TempK        0.10111E+05       5   0.36144E-05   0.74629E+01 0.95059E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5646e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.183          19.058       0.0072021      -0.0066306
v  Velocity[Y]             -15.799          15.144         0.21463         0.31056
v  Velocity[Z]             -25.463          11.991         -1.6486        -0.50754
v  ǁVelocityǁ         0.00060068          25.633          7.7096          6.6582
v  Pressure                 -511.6          205.17           28.65          32.736
v  k                   9.8802e-011            7.07         0.20862         0.44347
v  omega                     57.48     2.7321e+008     1.2912e+006           76893
v  TempK                    298.55          363.17          336.71          344.65
v  TurbVisc            2.4759e-018       0.0015864     5.1489e-005      0.00018255
v  CourantNb            0.00018025          1.5233         0.79251         0.97441
v  FourierNb             0.0037962               1          0.4108         0.16155
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038696     7.3804e-005      0.00020075

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.39          306.49
v  Yplus               0          2.9199         0.63184         0.48835


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68134          2.1173          1.2033           1.136


 INSTANT    0.704000000E-02   TIME STEP NUMBER             704
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924167E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13826E-01 0.46735E+01
   Friction velocity        uk    :  0.13826E-01 0.46695E+01
   Dimensionless distance   yplus :  0.93741E-02 0.29199E+01
   Friction thermal sca.    tstar :  0.12137E+01 0.18276E+03
   Rough dim-less th. sca.  tplus :  0.66407E-02 0.20684E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27580E+00      10   0.13996E-04   0.39302E+01 0.31099E+02 
c  Velocity[X]                                      0.15072E+01 
c  Velocity[Y]                                      0.10252E+01 
c  Velocity[Z]                                      0.13978E+01 
c  Pressure     0.15328E-04      18   0.27187E-03   0.15335E-01 0.16559E+02 
c  k            0.17434E-01      12   0.92757E-04   0.16978E+00 0.64778E+02 
c  omega        0.27922E+07       1   0.82840E-07   0.10386E+08 0.53665E+00 
c  TempK        0.10111E+05       5   0.36054E-05   0.74459E+01 0.94940E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5625e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.181          19.058       0.0072379      -0.0065897
v  Velocity[Y]             -15.724          15.148         0.21514         0.31115
v  Velocity[Z]             -25.465          11.986         -1.6485        -0.50753
v  ǁVelocityǁ         0.00058705          25.634           7.709          6.6572
v  Pressure                -511.58          205.24           28.73          32.824
v  k                   9.8797e-011          7.0834          0.2089         0.44411
v  omega                     57.48     2.7321e+008     1.2912e+006           76892
v  TempK                    298.56          363.17          336.72          344.67
v  TurbVisc            2.4758e-018       0.0016091     5.1564e-005      0.00018279
v  CourantNb            0.00018088          1.5238         0.79248         0.97438
v  FourierNb             0.0037967               1         0.41088         0.16175
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.003857     7.3809e-005      0.00020079

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.39          306.49
v  Yplus               0          2.9199         0.63181          0.4883


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56664          2.1178          1.2034          1.1361


 INSTANT    0.705000000E-02   TIME STEP NUMBER             705
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924144E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13823E-01 0.46733E+01
   Friction velocity        uk    :  0.13823E-01 0.46694E+01
   Dimensionless distance   yplus :  0.93724E-02 0.29199E+01
   Friction thermal sca.    tstar :  0.12135E+01 0.18279E+03
   Rough dim-less th. sca.  tplus :  0.66395E-02 0.20685E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27577E+00      10   0.13398E-04   0.39425E+01 0.31124E+02 
c  Velocity[X]                                      0.15173E+01 
c  Velocity[Y]                                      0.10302E+01 
c  Velocity[Z]                                      0.13951E+01 
c  Pressure     0.15763E-04      18   0.27422E-03   0.15772E-01 0.16942E+02 
c  k            0.17461E-01      12   0.92288E-04   0.17324E+00 0.65169E+02 
c  omega        0.27922E+07       1   0.82488E-07   0.10487E+08 0.53911E+00 
c  TempK        0.10111E+05       5   0.35977E-05   0.74328E+01 0.94842E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5606e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.18          19.058       0.0072716       -0.006548
v  Velocity[Y]             -15.659          15.153         0.21566         0.31175
v  Velocity[Z]             -25.466          11.981         -1.6484        -0.50751
v  ǁVelocityǁ         0.00057313          25.636          7.7085          6.6562
v  Pressure                -511.58          205.32          28.812          32.915
v  k                   9.8792e-011          7.1061         0.20917         0.44476
v  omega                    57.479     2.7321e+008     1.2912e+006           76892
v  TempK                    298.56          363.17          336.73          344.69
v  TurbVisc            2.4757e-018       0.0016305     5.1639e-005      0.00018303
v  CourantNb            0.00017763          1.5243         0.79246         0.97436
v  FourierNb             0.0037973               1         0.41096         0.16194
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038451     7.3815e-005      0.00020083

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.4          306.49
v  Yplus               0          2.9199         0.63177         0.48825


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.79548          2.1182          1.2034          1.1363


 INSTANT    0.706000000E-02   TIME STEP NUMBER             706
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924193E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13820E-01 0.46732E+01
   Friction velocity        uk    :  0.13820E-01 0.46692E+01
   Dimensionless distance   yplus :  0.93705E-02 0.29199E+01
   Friction thermal sca.    tstar :  0.12135E+01 0.18283E+03
   Rough dim-less th. sca.  tplus :  0.66381E-02 0.20685E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27574E+00      10   0.12923E-04   0.39595E+01 0.31186E+02 
c  Velocity[X]                                      0.15252E+01 
c  Velocity[Y]                                      0.10372E+01 
c  Velocity[Z]                                      0.13970E+01 
c  Pressure     0.15630E-04      18   0.28035E-03   0.15641E-01 0.16877E+02 
c  k            0.17489E-01      12   0.92476E-04   0.17579E+00 0.65491E+02 
c  omega        0.27922E+07       1   0.80650E-07   0.54709E+07 0.42613E+00 
c  TempK        0.10110E+05       5   0.35891E-05   0.74202E+01 0.94745E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5584e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.178          19.058       0.0073021      -0.0065071
v  Velocity[Y]             -15.634          15.158         0.21617         0.31234
v  Velocity[Z]             -25.468          11.975         -1.6483         -0.5075
v  ǁVelocityǁ         0.00055906          25.637           7.708          6.6551
v  Pressure                -511.58           205.4          28.895          33.006
v  k                   9.8787e-011          7.2461         0.20945          0.4454
v  omega                    57.479     2.7321e+008     1.2912e+006           76892
v  TempK                    298.56          363.17          336.74          344.71
v  TurbVisc            2.4756e-018       0.0016501     5.1714e-005      0.00018327
v  CourantNb            0.00017199          1.5248         0.79243         0.97433
v  FourierNb             0.0037979               1         0.41103         0.16214
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038341     7.3819e-005      0.00020086

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.4          306.49
v  Yplus               0          2.9199         0.63174          0.4882


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68837          2.1187          1.2035          1.1365


 INSTANT    0.707000000E-02   TIME STEP NUMBER             707
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924163E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13810E-01 0.46730E+01
   Friction velocity        uk    :  0.13810E-01 0.46690E+01
   Dimensionless distance   yplus :  0.93634E-02 0.29200E+01
   Friction thermal sca.    tstar :  0.12136E+01 0.18297E+03
   Rough dim-less th. sca.  tplus :  0.66331E-02 0.20685E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27571E+00      10   0.12858E-04   0.39761E+01 0.31247E+02 
c  Velocity[X]                                      0.15333E+01 
c  Velocity[Y]                                      0.10452E+01 
c  Velocity[Z]                                      0.13976E+01 
c  Pressure     0.15554E-04      18   0.27647E-03   0.15565E-01 0.16667E+02 
c  k            0.17516E-01      12   0.92793E-04   0.17801E+00 0.65788E+02 
c  omega        0.27922E+07       1   0.80694E-07   0.53333E+07 0.42336E+00 
c  TempK        0.10110E+05       5   0.35804E-05   0.74077E+01 0.94649E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5558e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.176          19.058       0.0073294      -0.0064671
v  Velocity[Y]             -15.644          15.162         0.21669         0.31294
v  Velocity[Z]              -25.47           11.97         -1.6482        -0.50749
v  ǁVelocityǁ         0.00054549          25.639          7.7074          6.6541
v  Pressure                -511.59          205.47          28.975          33.095
v  k                   9.8782e-011          7.3668         0.20973         0.44605
v  omega                    57.479     2.7321e+008     1.2912e+006           76892
v  TempK                    298.56          363.17          336.75          344.72
v  TurbVisc            2.4755e-018       0.0016689     5.1789e-005      0.00018351
v  CourantNb            0.00016691          1.5254          0.7924          0.9743
v  FourierNb             0.0037985               1         0.41111         0.16233
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038242     7.3824e-005       0.0002009

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.4          306.49
v  Yplus               0            2.92         0.63171         0.48815


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4748          2.1193          1.2035          1.1366


 INSTANT    0.708000000E-02   TIME STEP NUMBER             708
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924182E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13799E-01 0.46729E+01
   Friction velocity        uk    :  0.13799E-01 0.46689E+01
   Dimensionless distance   yplus :  0.93560E-02 0.29200E+01
   Friction thermal sca.    tstar :  0.12135E+01 0.18312E+03
   Rough dim-less th. sca.  tplus :  0.66278E-02 0.20686E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27568E+00      10   0.13114E-04   0.39968E+01 0.31327E+02 
c  Velocity[X]                                      0.15414E+01 
c  Velocity[Y]                                      0.10535E+01 
c  Velocity[Z]                                      0.14020E+01 
c  Pressure     0.15529E-04      18   0.27109E-03   0.15542E-01 0.17117E+02 
c  k            0.17544E-01      12   0.94965E-04   0.17930E+00 0.66048E+02 
c  omega        0.27922E+07       1   0.82554E-07   0.84156E+07 0.49538E+00 
c  TempK        0.10110E+05       5   0.35715E-05   0.73926E+01 0.94549E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5529e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.174          19.058       0.0073551       -0.006426
v  Velocity[Y]             -15.735          15.167          0.2172         0.31354
v  Velocity[Z]             -25.471          11.964         -1.6481        -0.50747
v  ǁVelocityǁ         0.00053206          25.641          7.7069          6.6531
v  Pressure                 -511.6          205.55          29.059          33.186
v  k                   9.8777e-011          7.4663         0.21001         0.44669
v  omega                    57.479     2.7321e+008     1.2912e+006           76892
v  TempK                    298.56          363.17          336.76          344.74
v  TurbVisc            2.4753e-018       0.0016875     5.1864e-005      0.00018375
v  CourantNb             0.0001624          1.5261         0.79238         0.97427
v  FourierNb             0.0037991               1         0.41118         0.16253
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038156     7.3829e-005      0.00020094

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.4          306.49
v  Yplus               0            2.92         0.63168          0.4881


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62249            2.12          1.2036          1.1368


 INSTANT    0.709000000E-02   TIME STEP NUMBER             709
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924188E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13782E-01 0.46727E+01
   Friction velocity        uk    :  0.13782E-01 0.46687E+01
   Dimensionless distance   yplus :  0.93446E-02 0.29201E+01
   Friction thermal sca.    tstar :  0.12135E+01 0.18334E+03
   Rough dim-less th. sca.  tplus :  0.66198E-02 0.20686E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27565E+00      10   0.13001E-04   0.40087E+01 0.31406E+02 
c  Velocity[X]                                      0.15490E+01 
c  Velocity[Y]                                      0.10638E+01 
c  Velocity[Z]                                      0.13959E+01 
c  Pressure     0.15192E-04      18   0.27059E-03   0.15205E-01 0.17689E+02 
c  k            0.17572E-01      12   0.94888E-04   0.18026E+00 0.66280E+02 
c  omega        0.27922E+07       1   0.86866E-07   0.20398E+08 0.71409E+00 
c  TempK        0.10109E+05       5   0.35624E-05   0.73794E+01 0.94462E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step       6.55e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.172          19.058       0.0073782      -0.0063834
v  Velocity[Y]             -15.776          15.171         0.21771         0.31414
v  Velocity[Z]             -25.473          11.959          -1.648        -0.50746
v  ǁVelocityǁ         0.00051899          25.642          7.7064           6.652
v  Pressure                -511.61          205.64          29.147          33.283
v  k                   9.8772e-011           7.528         0.21029         0.44734
v  omega                    57.479     2.7321e+008     1.2912e+006           76892
v  TempK                    298.56          363.17          336.77          344.76
v  TurbVisc            2.4752e-018       0.0017063      5.194e-005        0.000184
v  CourantNb            0.00016135          1.5267         0.79235         0.97424
v  FourierNb             0.0037996               1         0.41126         0.16272
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038077     7.3835e-005      0.00020098

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.4           306.5
v  Yplus               0          2.9201         0.63164         0.48805


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67044          2.1207          1.2036           1.137


 INSTANT    0.710000000E-02   TIME STEP NUMBER             710
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924198E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13769E-01 0.46725E+01
   Friction velocity        uk    :  0.13769E-01 0.46686E+01
   Dimensionless distance   yplus :  0.93357E-02 0.29201E+01
   Friction thermal sca.    tstar :  0.12135E+01 0.18351E+03
   Rough dim-less th. sca.  tplus :  0.66134E-02 0.20686E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27562E+00      10   0.13026E-04   0.40296E+01 0.31482E+02 
c  Velocity[X]                                      0.15564E+01 
c  Velocity[Y]                                      0.10753E+01 
c  Velocity[Z]                                      0.13978E+01 
c  Pressure     0.15295E-04      18   0.27178E-03   0.15309E-01 0.17557E+02 
c  k            0.17600E-01      12   0.96191E-04   0.18125E+00 0.66498E+02 
c  omega        0.27922E+07       1   0.84516E-07   0.13582E+08 0.60033E+00 
c  TempK        0.10109E+05       5   0.35544E-05   0.73675E+01 0.94366E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5477e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.17          19.058        0.007396      -0.0063385
v  Velocity[Y]             -15.686          15.175         0.21823         0.31474
v  Velocity[Z]             -25.475          11.953          -1.648        -0.50745
v  ǁVelocityǁ         0.00050545          25.644          7.7059           6.651
v  Pressure                -511.64          205.72          29.234          33.378
v  k                   9.8768e-011          7.5423         0.21057         0.44799
v  omega                    57.479     2.7321e+008     1.2912e+006           76892
v  TempK                    298.56          363.17          336.78          344.78
v  TurbVisc            2.4751e-018       0.0017249     5.2016e-005      0.00018424
v  CourantNb            0.00016723          1.5273         0.79233         0.97421
v  FourierNb             0.0038002               1         0.41133         0.16292
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039979      7.384e-005      0.00020102

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.4           306.5
v  Yplus               0          2.9201         0.63161           0.488


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78566          2.1213          1.2037          1.1371


 INSTANT    0.711000000E-02   TIME STEP NUMBER             711
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924222E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13769E-01 0.46724E+01
   Friction velocity        uk    :  0.13768E-01 0.46684E+01
   Dimensionless distance   yplus :  0.93353E-02 0.29202E+01
   Friction thermal sca.    tstar :  0.12136E+01 0.18352E+03
   Rough dim-less th. sca.  tplus :  0.66132E-02 0.20687E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27559E+00      10   0.13256E-04   0.40453E+01 0.31513E+02 
c  Velocity[X]                                      0.15646E+01 
c  Velocity[Y]                                      0.10814E+01 
c  Velocity[Z]                                      0.13993E+01 
c  Pressure     0.15409E-04      18   0.27948E-03   0.15425E-01 0.18153E+02 
c  k            0.17628E-01      12   0.97885E-04   0.18292E+00 0.66743E+02 
c  omega        0.27922E+07       1   0.83470E-07   0.98067E+07 0.52443E+00 
c  TempK        0.10108E+05       5   0.35467E-05   0.73597E+01 0.94298E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5455e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.168          19.058       0.0074094      -0.0062941
v  Velocity[Y]             -15.623           15.18         0.21875         0.31534
v  Velocity[Z]             -25.477          11.947         -1.6479        -0.50743
v  ǁVelocityǁ         0.00049258          25.646          7.7053          6.6499
v  Pressure                -511.68          205.81          29.324          33.477
v  k                   9.8763e-011          7.5175         0.21085         0.44864
v  omega                    57.479     2.7321e+008     1.2912e+006           76891
v  TempK                    298.56          363.17          336.79          344.79
v  TurbVisc             2.475e-018        0.001748     5.2092e-005      0.00018448
v  CourantNb            0.00017451          1.5278          0.7923         0.97418
v  FourierNb             0.0038007               1         0.41141         0.16311
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0042271     7.3844e-005      0.00020105

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.4           306.5
v  Yplus               0          2.9202         0.63158         0.48795


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.80845          2.1218          1.2037          1.1373


 INSTANT    0.712000000E-02   TIME STEP NUMBER             712
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924198E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13768E-01 0.46723E+01
   Friction velocity        uk    :  0.13768E-01 0.46683E+01
   Dimensionless distance   yplus :  0.93350E-02 0.29202E+01
   Friction thermal sca.    tstar :  0.12140E+01 0.18353E+03
   Rough dim-less th. sca.  tplus :  0.66130E-02 0.20687E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27556E+00      10   0.15266E-04   0.40637E+01 0.31593E+02 
c  Velocity[X]                                      0.15752E+01 
c  Velocity[Y]                                      0.10937E+01 
c  Velocity[Z]                                      0.13948E+01 
c  Pressure     0.15423E-04      18   0.27518E-03   0.15442E-01 0.17121E+02 
c  k            0.17655E-01      12   0.98213E-04   0.18548E+00 0.67031E+02 
c  omega        0.27922E+07       1   0.82930E-07   0.87897E+07 0.50594E+00 
c  TempK        0.10108E+05       5   0.35379E-05   0.73496E+01 0.94217E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.543e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.166          19.058       0.0074196      -0.0062502
v  Velocity[Y]             -15.611          15.185         0.21927         0.31595
v  Velocity[Z]             -25.479          11.941         -1.6478        -0.50742
v  ǁVelocityǁ         0.00047986          25.647          7.7048          6.6489
v  Pressure                -511.73          205.89          29.408          33.569
v  k                   9.8758e-011          7.4942         0.21113         0.44929
v  omega                    57.479     2.7321e+008     1.2912e+006           76891
v  TempK                    298.56          363.17           336.8          344.81
v  TurbVisc            2.4749e-018       0.0017744     5.2168e-005      0.00018473
v  CourantNb            0.00017508          1.5283         0.79227         0.97416
v  FourierNb             0.0038012               1         0.41148         0.16331
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0044358     7.3849e-005      0.00020109

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.4           306.5
v  Yplus               0          2.9202         0.63154          0.4879


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76331          2.1224          1.2038          1.1375


 INSTANT    0.713000000E-02   TIME STEP NUMBER             713
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924142E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13759E-01 0.46721E+01
   Friction velocity        uk    :  0.13759E-01 0.46682E+01
   Dimensionless distance   yplus :  0.93289E-02 0.29202E+01
   Friction thermal sca.    tstar :  0.12139E+01 0.18365E+03
   Rough dim-less th. sca.  tplus :  0.66087E-02 0.20687E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27553E+00      10   0.15298E-04   0.40762E+01 0.31611E+02 
c  Velocity[X]                                      0.15833E+01 
c  Velocity[Y]                                      0.11002E+01 
c  Velocity[Z]                                      0.13927E+01 
c  Pressure     0.15699E-04      18   0.27419E-03   0.15720E-01 0.17111E+02 
c  k            0.17682E-01      12   0.99447E-04   0.19072E+00 0.67440E+02 
c  omega        0.27922E+07       1   0.83455E-07   0.93522E+07 0.52045E+00 
c  TempK        0.10107E+05       5   0.35305E-05   0.73377E+01 0.94141E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5402e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.163          19.059       0.0074255      -0.0062056
v  Velocity[Y]             -15.629          15.189         0.21979         0.31655
v  Velocity[Z]              -25.48          11.935         -1.6477        -0.50739
v  ǁVelocityǁ         0.00046775          25.649          7.7043          6.6479
v  Pressure                -511.79          205.97          29.492          33.661
v  k                   9.8753e-011          7.5839         0.21141         0.44993
v  omega                    57.479      2.732e+008     1.2912e+006           76891
v  TempK                    298.56          363.17          336.81          344.83
v  TurbVisc            2.4747e-018       0.0018093     5.2246e-005      0.00018498
v  CourantNb            0.00017609           1.529         0.79224         0.97412
v  FourierNb             0.0038018               1         0.41156         0.16351
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045691     7.3855e-005      0.00020112

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.4           306.5
v  Yplus               0          2.9202         0.63151         0.48785


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62813           2.123          1.2038          1.1376


 INSTANT    0.714000000E-02   TIME STEP NUMBER             714
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924158E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13753E-01 0.46720E+01
   Friction velocity        uk    :  0.13753E-01 0.46680E+01
   Dimensionless distance   yplus :  0.93246E-02 0.29203E+01
   Friction thermal sca.    tstar :  0.12138E+01 0.18373E+03
   Rough dim-less th. sca.  tplus :  0.66056E-02 0.20687E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27550E+00      10   0.13564E-04   0.40980E+01 0.31676E+02 
c  Velocity[X]                                      0.15929E+01 
c  Velocity[Y]                                      0.11074E+01 
c  Velocity[Z]                                      0.13977E+01 
c  Pressure     0.16017E-04      17   0.27277E-03   0.16039E-01 0.17330E+02 
c  k            0.17709E-01      12   0.10217E-03   0.19517E+00 0.67839E+02 
c  omega        0.27922E+07       1   0.84277E-07   0.10281E+08 0.53112E+00 
c  TempK        0.10107E+05       5   0.35217E-05   0.73254E+01 0.94075E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.537e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.161          19.059       0.0074264      -0.0061616
v  Velocity[Y]             -15.737          15.194         0.22031         0.31716
v  Velocity[Z]             -25.482          11.929         -1.6476        -0.50738
v  ǁVelocityǁ         0.00045541          25.651          7.7037          6.6468
v  Pressure                -511.85          206.05          29.578          33.755
v  k                   9.8749e-011          7.6658          0.2117         0.45056
v  omega                    57.479      2.732e+008     1.2912e+006           76891
v  TempK                    298.56          363.17          336.82          344.84
v  TurbVisc            2.4746e-018       0.0018442     5.2323e-005      0.00018523
v  CourantNb            0.00015761          1.5298         0.79221         0.97409
v  FourierNb             0.0038023               1         0.41164         0.16371
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045725      7.386e-005      0.00020116

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.4           306.5
v  Yplus               0          2.9203         0.63147          0.4878


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53191          2.1238          1.2039          1.1378


 INSTANT    0.715000000E-02   TIME STEP NUMBER             715
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924176E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13738E-01 0.46718E+01
   Friction velocity        uk    :  0.13738E-01 0.46679E+01
   Dimensionless distance   yplus :  0.93145E-02 0.29203E+01
   Friction thermal sca.    tstar :  0.12138E+01 0.18393E+03
   Rough dim-less th. sca.  tplus :  0.65984E-02 0.20688E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27547E+00      10   0.13487E-04   0.41195E+01 0.31758E+02 
c  Velocity[X]                                      0.16038E+01 
c  Velocity[Y]                                      0.11198E+01 
c  Velocity[Z]                                      0.13958E+01 
c  Pressure     0.16117E-04      18   0.27716E-03   0.16140E-01 0.16705E+02 
c  k            0.17735E-01      12   0.10354E-03   0.19585E+00 0.67950E+02 
c  omega        0.27922E+07       1   0.86958E-07   0.18379E+08 0.68240E+00 
c  TempK        0.10107E+05       5   0.35141E-05   0.73130E+01 0.94002E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.534e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.159          19.059       0.0074262      -0.0061171
v  Velocity[Y]             -15.765          15.198         0.22083         0.31777
v  Velocity[Z]             -25.484          11.923         -1.6475        -0.50736
v  ǁVelocityǁ         0.00044382          25.652          7.7032          6.6458
v  Pressure                -511.93          206.13          29.659          33.843
v  k                   9.8744e-011          7.7353         0.21198          0.4512
v  omega                    57.479      2.732e+008     1.2912e+006           76891
v  TempK                    298.56          363.17          336.83          344.86
v  TurbVisc            2.4745e-018       0.0018779       5.24e-005      0.00018547
v  CourantNb            0.00017887          1.5304         0.79218         0.97406
v  FourierNb             0.0038028               1         0.41172         0.16391
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045764     7.3866e-005       0.0002012

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.4           306.5
v  Yplus               0          2.9203         0.63144         0.48775


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56275          2.1245          1.2039           1.138


 INSTANT    0.716000000E-02   TIME STEP NUMBER             716
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924111E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13728E-01 0.46717E+01
   Friction velocity        uk    :  0.13728E-01 0.46677E+01
   Dimensionless distance   yplus :  0.93077E-02 0.29204E+01
   Friction thermal sca.    tstar :  0.12138E+01 0.18407E+03
   Rough dim-less th. sca.  tplus :  0.65937E-02 0.20688E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27544E+00      10   0.13291E-04   0.41350E+01 0.31812E+02 
c  Velocity[X]                                      0.16109E+01 
c  Velocity[Y]                                      0.11292E+01 
c  Velocity[Z]                                      0.13950E+01 
c  Pressure     0.16149E-04      18   0.27645E-03   0.16173E-01 0.16706E+02 
c  k            0.17760E-01      12   0.10387E-03   0.19552E+00 0.67946E+02 
c  omega        0.27922E+07       1   0.83441E-07   0.82638E+07 0.49406E+00 
c  TempK        0.10106E+05       5   0.35064E-05   0.73059E+01 0.93940E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5317e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.157          19.059       0.0074214      -0.0060742
v  Velocity[Y]              -15.68          15.202         0.22135         0.31838
v  Velocity[Z]             -25.486          11.917         -1.6474        -0.50734
v  ǁVelocityǁ         0.00043223          25.654          7.7027          6.6447
v  Pressure                -512.01          206.21           29.74          33.933
v  k                   9.8739e-011          7.7911         0.21226         0.45183
v  omega                    57.479      2.732e+008     1.2912e+006           76890
v  TempK                    298.56          363.17          336.84          344.88
v  TurbVisc            2.4744e-018       0.0019093     5.2478e-005      0.00018571
v  CourantNb            0.00018039           1.531         0.79216         0.97404
v  FourierNb             0.0038033               1          0.4118         0.16411
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045804     7.3872e-005      0.00020124

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.4           306.5
v  Yplus               0          2.9204         0.63141          0.4877


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51367          2.1251           1.204          1.1381


 INSTANT    0.717000000E-02   TIME STEP NUMBER             717
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924103E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13729E-01 0.46715E+01
   Friction velocity        uk    :  0.13729E-01 0.46676E+01
   Dimensionless distance   yplus :  0.93084E-02 0.29204E+01
   Friction thermal sca.    tstar :  0.12138E+01 0.18405E+03
   Rough dim-less th. sca.  tplus :  0.65941E-02 0.20689E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27541E+00      10   0.13211E-04   0.41526E+01 0.31849E+02 
c  Velocity[X]                                      0.16185E+01 
c  Velocity[Y]                                      0.11329E+01 
c  Velocity[Z]                                      0.14012E+01 
c  Pressure     0.16410E-04      18   0.27637E-03   0.16436E-01 0.16778E+02 
c  k            0.17786E-01      12   0.10444E-03   0.19479E+00 0.67827E+02 
c  omega        0.27922E+07       1   0.83700E-07   0.10220E+08 0.53499E+00 
c  TempK        0.10106E+05       5   0.34993E-05   0.72985E+01 0.93881E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5295e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.155           19.06       0.0074163      -0.0060297
v  Velocity[Y]             -15.623          15.207         0.22186         0.31899
v  Velocity[Z]             -25.488          11.917         -1.6474        -0.50733
v  ǁVelocityǁ          0.0004214          25.656          7.7021          6.6437
v  Pressure                -512.12          206.28          29.821          34.023
v  k                   9.8735e-011          7.8281         0.21254         0.45246
v  omega                    57.479      2.732e+008     1.2912e+006           76890
v  TempK                    298.57          363.17          336.85          344.89
v  TurbVisc            2.4743e-018       0.0019385     5.2556e-005      0.00018596
v  CourantNb            0.00018337          1.5315         0.79213         0.97401
v  FourierNb             0.0038038               1         0.41187         0.16431
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045839     7.3878e-005      0.00020128

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.4           306.5
v  Yplus               0          2.9204         0.63137         0.48765


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47962          2.1256           1.204          1.1383


 INSTANT    0.718000000E-02   TIME STEP NUMBER             718
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924298E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13731E-01 0.46714E+01
   Friction velocity        uk    :  0.13731E-01 0.46674E+01
   Dimensionless distance   yplus :  0.93099E-02 0.29205E+01
   Friction thermal sca.    tstar :  0.12138E+01 0.18402E+03
   Rough dim-less th. sca.  tplus :  0.65952E-02 0.20689E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27538E+00      10   0.13184E-04   0.41604E+01 0.31896E+02 
c  Velocity[X]                                      0.16260E+01 
c  Velocity[Y]                                      0.11395E+01 
c  Velocity[Z]                                      0.13949E+01 
c  Pressure     0.16229E-04      18   0.27995E-03   0.16256E-01 0.15873E+02 
c  k            0.17811E-01      12   0.10521E-03   0.19387E+00 0.67660E+02 
c  omega        0.27922E+07       1   0.82070E-07   0.54370E+07 0.42518E+00 
c  TempK        0.10105E+05       5   0.34928E-05   0.72926E+01 0.93828E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5269e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.153           19.06       0.0074084       -0.005983
v  Velocity[Y]             -15.608          15.212         0.22238          0.3196
v  Velocity[Z]              -25.49          11.922         -1.6473        -0.50732
v  ǁVelocityǁ          0.0004107          25.658          7.7016          6.6426
v  Pressure                -512.23          206.36          29.896          34.106
v  k                    9.873e-011          7.8395         0.21282         0.45309
v  omega                    57.479      2.732e+008     1.2912e+006           76890
v  TempK                    298.57          363.17          336.86          344.91
v  TurbVisc            2.4741e-018       0.0019666     5.2634e-005       0.0001862
v  CourantNb            0.00018478          1.5321          0.7921         0.97398
v  FourierNb             0.0038042               1         0.41195         0.16451
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045866     7.3883e-005      0.00020132

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.41           306.5
v  Yplus               0          2.9205         0.63133          0.4876


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50464          2.1262          1.2041          1.1385


 INSTANT    0.719000000E-02   TIME STEP NUMBER             719
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924125E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13725E-01 0.46713E+01
   Friction velocity        uk    :  0.13725E-01 0.46673E+01
   Dimensionless distance   yplus :  0.93056E-02 0.29206E+01
   Friction thermal sca.    tstar :  0.12138E+01 0.18411E+03
   Rough dim-less th. sca.  tplus :  0.65922E-02 0.20689E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27535E+00      10   0.13172E-04   0.41766E+01 0.31952E+02 
c  Velocity[X]                                      0.16343E+01 
c  Velocity[Y]                                      0.11468E+01 
c  Velocity[Z]                                      0.13955E+01 
c  Pressure     0.16435E-04      18   0.28332E-03   0.16464E-01 0.16994E+02 
c  k            0.17835E-01      12   0.10594E-03   0.19298E+00 0.67464E+02 
c  omega        0.27922E+07       1   0.82096E-07   0.52997E+07 0.42213E+00 
c  TempK        0.10105E+05       5   0.34871E-05   0.72893E+01 0.93783E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5239e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.151           19.06       0.0073971      -0.0059375
v  Velocity[Y]             -15.624          15.216         0.22289          0.3202
v  Velocity[Z]             -25.492          11.926         -1.6472         -0.5073
v  ǁVelocityǁ         0.00040064           25.66          7.7011          6.6416
v  Pressure                -512.35          206.44          29.979          34.197
v  k                   9.8725e-011          7.8217          0.2131         0.45372
v  omega                    57.479      2.732e+008     1.2912e+006           76890
v  TempK                    298.57          363.17          336.87          344.93
v  TurbVisc             2.474e-018       0.0019814     5.2712e-005      0.00018644
v  CourantNb            0.00018998          1.5328         0.79207         0.97395
v  FourierNb             0.0038047               1         0.41203         0.16471
v  total_pressure      1.0081e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045342     7.3889e-005      0.00020136

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.41           306.5
v  Yplus               0          2.9206          0.6313         0.48755


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42249          2.1269          1.2041          1.1387


 INSTANT    0.720000000E-02   TIME STEP NUMBER             720
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924274E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13720E-01 0.46711E+01
   Friction velocity        uk    :  0.13720E-01 0.46672E+01
   Dimensionless distance   yplus :  0.93025E-02 0.29206E+01
   Friction thermal sca.    tstar :  0.12138E+01 0.18417E+03
   Rough dim-less th. sca.  tplus :  0.65900E-02 0.20690E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27532E+00      10   0.13179E-04   0.41931E+01 0.32044E+02 
c  Velocity[X]                                      0.16415E+01 
c  Velocity[Y]                                      0.11537E+01 
c  Velocity[Z]                                      0.13979E+01 
c  Pressure     0.16171E-04      18   0.27638E-03   0.16200E-01 0.16775E+02 
c  k            0.17860E-01      12   0.10664E-03   0.19151E+00 0.67185E+02 
c  omega        0.27922E+07       1   0.86351E-07   0.12903E+08 0.58314E+00 
c  TempK        0.10104E+05       5   0.34808E-05   0.72888E+01 0.93758E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5206e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.148           19.06       0.0073844       -0.005893
v  Velocity[Y]             -15.715          15.221         0.22341         0.32081
v  Velocity[Z]             -25.494           11.93         -1.6472        -0.50727
v  ǁVelocityǁ         0.00039087          25.662          7.7006          6.6406
v  Pressure                -512.48          206.52           30.06          34.285
v  k                   9.8721e-011          7.7742         0.21338         0.45435
v  omega                    57.479      2.732e+008     1.2912e+006           76890
v  TempK                    298.57          363.17          336.88          344.94
v  TurbVisc            2.4739e-018       0.0019774      5.279e-005      0.00018668
v  CourantNb            0.00019078          1.5336         0.79205         0.97392
v  FourierNb             0.0038052               1          0.4121         0.16491
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0043009     7.3894e-005      0.00020139

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.41           306.5
v  Yplus               0          2.9206         0.63127         0.48751


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42861          2.1277          1.2041          1.1388


 INSTANT    0.721000000E-02   TIME STEP NUMBER             721
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924150E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13710E-01 0.46710E+01
   Friction velocity        uk    :  0.13710E-01 0.46670E+01
   Dimensionless distance   yplus :  0.92954E-02 0.29207E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.18431E+03
   Rough dim-less th. sca.  tplus :  0.65849E-02 0.20690E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27529E+00      10   0.13085E-04   0.42056E+01 0.32153E+02 
c  Velocity[X]                                      0.16490E+01 
c  Velocity[Y]                                      0.11653E+01 
c  Velocity[Z]                                      0.13913E+01 
c  Pressure     0.15966E-04      18   0.27666E-03   0.15995E-01 0.17172E+02 
c  k            0.17885E-01      12   0.10615E-03   0.18914E+00 0.66815E+02 
c  omega        0.27922E+07       1   0.91367E-07   0.27793E+08 0.82017E+00 
c  TempK        0.10104E+05       5   0.34734E-05   0.72840E+01 0.93710E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5174e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.146          19.061       0.0073704      -0.0058478
v  Velocity[Y]             -15.756          15.225         0.22393         0.32143
v  Velocity[Z]             -25.496          11.934         -1.6471        -0.50725
v  ǁVelocityǁ         0.00038205          25.664          7.7001          6.6395
v  Pressure                -512.61           206.6          30.145          34.378
v  k                   9.8716e-011           7.699         0.21366         0.45498
v  omega                    57.479      2.732e+008     1.2912e+006           76889
v  TempK                    298.57          363.17          336.89          344.96
v  TurbVisc            2.4738e-018       0.0019705     5.2868e-005      0.00018693
v  CourantNb            0.00019141          1.5344         0.79202         0.97389
v  FourierNb             0.0038056               1         0.41218         0.16511
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0040367       7.39e-005      0.00020143

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.41           306.5
v  Yplus               0          2.9207         0.63123         0.48746


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47323          2.1285          1.2042           1.139


 INSTANT    0.722000000E-02   TIME STEP NUMBER             722
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924205E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13704E-01 0.46709E+01
   Friction velocity        uk    :  0.13704E-01 0.46669E+01
   Dimensionless distance   yplus :  0.92914E-02 0.29207E+01
   Friction thermal sca.    tstar :  0.12142E+01 0.18439E+03
   Rough dim-less th. sca.  tplus :  0.65821E-02 0.20690E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27526E+00      10   0.13331E-04   0.42129E+01 0.32173E+02 
c  Velocity[X]                                      0.16530E+01 
c  Velocity[Y]                                      0.11686E+01 
c  Velocity[Z]                                      0.13913E+01 
c  Pressure     0.16030E-04      18   0.28044E-03   0.16060E-01 0.15118E+02 
c  k            0.17910E-01      12   0.10554E-03   0.18641E+00 0.66398E+02 
c  omega        0.27922E+07       1   0.86184E-07   0.13776E+08 0.60565E+00 
c  TempK        0.10104E+05       5   0.34659E-05   0.72795E+01 0.93650E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5147e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.144          19.061       0.0073542       -0.005799
v  Velocity[Y]             -15.669          15.229         0.22444         0.32204
v  Velocity[Z]             -25.498          11.937          -1.647        -0.50723
v  ǁVelocityǁ         0.00037305          25.665          7.6995          6.6385
v  Pressure                -512.77          206.66          30.213          34.454
v  k                   9.8712e-011          7.5996         0.21394          0.4556
v  omega                    57.479      2.732e+008     1.2912e+006           76889
v  TempK                    298.57          363.17           336.9          344.98
v  TurbVisc            2.4737e-018       0.0019616     5.2947e-005      0.00018717
v  CourantNb              0.000192           1.535         0.79199         0.97386
v  FourierNb              0.003806               1         0.41226         0.16531
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037433     7.3905e-005      0.00020147

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.41          306.51
v  Yplus               0          2.9207          0.6312         0.48742


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5404          2.1291          1.2042          1.1392


 INSTANT    0.723000000E-02   TIME STEP NUMBER             723
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924073E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13705E-01 0.46707E+01
   Friction velocity        uk    :  0.13705E-01 0.46668E+01
   Dimensionless distance   yplus :  0.92924E-02 0.29207E+01
   Friction thermal sca.    tstar :  0.12140E+01 0.18437E+03
   Rough dim-less th. sca.  tplus :  0.65828E-02 0.20691E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27523E+00      10   0.13949E-04   0.42191E+01 0.32160E+02 
c  Velocity[X]                                      0.16590E+01 
c  Velocity[Y]                                      0.11683E+01 
c  Velocity[Z]                                      0.13918E+01 
c  Pressure     0.16029E-04      18   0.28514E-03   0.16058E-01 0.15564E+02 
c  k            0.17934E-01      12   0.10500E-03   0.18411E+00 0.66005E+02 
c  omega        0.27922E+07       1   0.83554E-07   0.64505E+07 0.45363E+00 
c  TempK        0.10103E+05       5   0.34584E-05   0.72777E+01 0.93607E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5122e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.142          19.061       0.0073347      -0.0057517
v  Velocity[Y]             -15.606          15.234         0.22496         0.32265
v  Velocity[Z]               -25.5           11.94          -1.647        -0.50721
v  ǁVelocityǁ         0.00036558          25.667           7.699          6.6374
v  Pressure                -512.95          206.73          30.285          34.534
v  k                   9.8707e-011          7.6437         0.21422         0.45622
v  omega                    57.479      2.732e+008     1.2912e+006           76889
v  TempK                    298.57          363.17          336.91          344.99
v  TurbVisc            2.4736e-018        0.001951     5.3025e-005      0.00018741
v  CourantNb            0.00019267          1.5356         0.79196         0.97383
v  FourierNb             0.0038064               1         0.41234         0.16551
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034533     7.3911e-005      0.00020151

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.41          306.51
v  Yplus               0          2.9207         0.63116         0.48738


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6571          2.1297          1.2043          1.1393


 INSTANT    0.724000000E-02   TIME STEP NUMBER             724
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924182E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13710E-01 0.46706E+01
   Friction velocity        uk    :  0.13710E-01 0.46667E+01
   Dimensionless distance   yplus :  0.92956E-02 0.29208E+01
   Friction thermal sca.    tstar :  0.12140E+01 0.18431E+03
   Rough dim-less th. sca.  tplus :  0.65850E-02 0.20691E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27520E+00      10   0.13565E-04   0.42265E+01 0.32197E+02 
c  Velocity[X]                                      0.16647E+01 
c  Velocity[Y]                                      0.11724E+01 
c  Velocity[Z]                                      0.13895E+01 
c  Pressure     0.15830E-04      18   0.28634E-03   0.15860E-01 0.14984E+02 
c  k            0.17958E-01      12   0.10478E-03   0.18254E+00 0.65646E+02 
c  omega        0.27922E+07       1   0.83581E-07   0.60542E+07 0.44750E+00 
c  TempK        0.10103E+05       5   0.34525E-05   0.72778E+01 0.93564E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5095e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.14          19.062       0.0073113      -0.0057056
v  Velocity[Y]             -15.595          15.238         0.22548         0.32327
v  Velocity[Z]             -25.502          11.942         -1.6469        -0.50718
v  ǁVelocityǁ         0.00035818          25.669          7.6985          6.6364
v  Pressure                -513.13           206.8          30.352           34.61
v  k                   9.8703e-011          7.7197         0.21449         0.45684
v  omega                    57.479      2.732e+008     1.2912e+006           76889
v  TempK                    298.57          363.17          336.91          345.01
v  TurbVisc            2.4735e-018       0.0019664     5.3103e-005      0.00018765
v  CourantNb            0.00019323          1.5362         0.79194         0.97381
v  FourierNb             0.0038068               1         0.41241         0.16571
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.003453     7.3915e-005      0.00020155

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.41          306.51
v  Yplus               0          2.9208         0.63112         0.48733


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75095          2.1304          1.2043          1.1395


 INSTANT    0.725000000E-02   TIME STEP NUMBER             725
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924086E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13705E-01 0.46705E+01
   Friction velocity        uk    :  0.13705E-01 0.46665E+01
   Dimensionless distance   yplus :  0.92922E-02 0.29208E+01
   Friction thermal sca.    tstar :  0.12141E+01 0.18437E+03
   Rough dim-less th. sca.  tplus :  0.65827E-02 0.20691E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27517E+00      10   0.13245E-04   0.42348E+01 0.32227E+02 
c  Velocity[X]                                      0.16706E+01 
c  Velocity[Y]                                      0.11761E+01 
c  Velocity[Z]                                      0.13881E+01 
c  Pressure     0.15827E-04      18   0.28638E-03   0.15857E-01 0.15186E+02 
c  k            0.17981E-01      12   0.10465E-03   0.18084E+00 0.65251E+02 
c  omega        0.27922E+07       1   0.83908E-07   0.61849E+07 0.45336E+00 
c  TempK        0.10102E+05       5   0.34480E-05   0.72740E+01 0.93520E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5064e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.138          19.062       0.0072858      -0.0056593
v  Velocity[Y]             -15.613          15.243           0.226         0.32389
v  Velocity[Z]             -25.504          11.944         -1.6468        -0.50715
v  ǁVelocityǁ          0.0003519          25.671           7.698          6.6353
v  Pressure                -513.33          206.87          30.422          34.688
v  k                   9.8699e-011          7.7767         0.21477         0.45746
v  omega                    57.479      2.732e+008     1.2912e+006           76889
v  TempK                    298.57          363.17          336.92          345.03
v  TurbVisc            2.4734e-018       0.0019455     5.3182e-005      0.00018789
v  CourantNb            0.00019386           1.537         0.79191         0.97378
v  FourierNb             0.0038072               1         0.41249         0.16591
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034526     7.3919e-005      0.00020159

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.41          306.51
v  Yplus               0          2.9208         0.63109         0.48729


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71893          2.1311          1.2044          1.1397


 INSTANT    0.726000000E-02   TIME STEP NUMBER             726
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924148E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13704E-01 0.46703E+01
   Friction velocity        uk    :  0.13704E-01 0.46664E+01
   Dimensionless distance   yplus :  0.92919E-02 0.29209E+01
   Friction thermal sca.    tstar :  0.12141E+01 0.18438E+03
   Rough dim-less th. sca.  tplus :  0.65824E-02 0.20692E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27514E+00      10   0.12922E-04   0.42494E+01 0.32280E+02 
c  Velocity[X]                                      0.16758E+01 
c  Velocity[Y]                                      0.11801E+01 
c  Velocity[Z]                                      0.13936E+01 
c  Pressure     0.16121E-04      18   0.27919E-03   0.16154E-01 0.15339E+02 
c  k            0.18003E-01      12   0.10339E-03   0.17828E+00 0.64774E+02 
c  omega        0.27922E+07       1   0.88503E-07   0.14550E+08 0.61983E+00 
c  TempK        0.10102E+05       5   0.34410E-05   0.72709E+01 0.93503E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5029e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.135          19.063       0.0072559      -0.0056134
v  Velocity[Y]              -15.74          15.247         0.22652         0.32452
v  Velocity[Z]             -25.506          12.516         -1.6468        -0.50713
v  ǁVelocityǁ          0.0003461          25.673          7.6975          6.6343
v  Pressure                -513.52          206.93          30.493          34.767
v  k                   9.8694e-011          7.8165         0.21504         0.45807
v  omega                     57.48      2.732e+008     1.2912e+006           76888
v  TempK                    298.57          363.17          336.93          345.04
v  TurbVisc            2.4732e-018       0.0019173     5.3261e-005      0.00018813
v  CourantNb            0.00019443          1.5378         0.79188         0.97375
v  FourierNb             0.0038076               1         0.41256         0.16611
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034521     7.3922e-005      0.00020162

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.41          306.51
v  Yplus               0          2.9209         0.63105         0.48725


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52749          2.1319          1.2044          1.1399


 INSTANT    0.727000000E-02   TIME STEP NUMBER             727
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924184E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13694E-01 0.46702E+01
   Friction velocity        uk    :  0.13694E-01 0.46663E+01
   Dimensionless distance   yplus :  0.92846E-02 0.29210E+01
   Friction thermal sca.    tstar :  0.12141E+01 0.18453E+03
   Rough dim-less th. sca.  tplus :  0.65773E-02 0.20692E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27512E+00      10   0.13064E-04   0.42696E+01 0.32355E+02 
c  Velocity[X]                                      0.16817E+01 
c  Velocity[Y]                                      0.11876E+01 
c  Velocity[Z]                                      0.14002E+01 
c  Pressure     0.15933E-04      18   0.27477E-03   0.15966E-01 0.14841E+02 
c  k            0.18025E-01      12   0.99980E-04   0.17408E+00 0.64168E+02 
c  omega        0.27922E+07       1   0.87746E-07   0.13612E+08 0.60853E+00 
c  TempK        0.10101E+05       5   0.34352E-05   0.72666E+01 0.93450E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step        6.5e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.133          19.063       0.0072295      -0.0055657
v  Velocity[Y]             -15.713          15.251         0.22704         0.32514
v  Velocity[Z]             -25.508          11.947         -1.6467         -0.5071
v  ǁVelocityǁ         0.00034098          25.675           7.697          6.6332
v  Pressure                -513.74          206.99          30.559          34.841
v  k                    9.869e-011          7.8413         0.21532         0.45868
v  omega                     57.48      2.732e+008     1.2912e+006           76888
v  TempK                    298.57          363.17          336.94          345.06
v  TurbVisc            2.4731e-018       0.0018867     5.3339e-005      0.00018837
v  CourantNb            0.00019502          1.5385         0.79186         0.97372
v  FourierNb              0.003808               1         0.41264         0.16631
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034516     7.3926e-005      0.00020166

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.41          306.51
v  Yplus               0           2.921         0.63102         0.48721


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60012          2.1326          1.2045            1.14


 INSTANT    0.728000000E-02   TIME STEP NUMBER             728
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924111E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13460E-01 0.46701E+01
   Friction velocity        uk    :  0.13460E-01 0.46662E+01
   Dimensionless distance   yplus :  0.91264E-02 0.29210E+01
   Friction thermal sca.    tstar :  0.12141E+01 0.18479E+03
   Rough dim-less th. sca.  tplus :  0.64652E-02 0.20693E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27509E+00      10   0.13148E-04   0.42610E+01 0.32332E+02 
c  Velocity[X]                                      0.16854E+01 
c  Velocity[Y]                                      0.11876E+01 
c  Velocity[Z]                                      0.13880E+01 
c  Pressure     0.15776E-04      18   0.27135E-03   0.15811E-01 0.15340E+02 
c  k            0.18048E-01      12   0.96320E-04   0.16995E+00 0.63545E+02 
c  omega        0.27922E+07       1   0.85248E-07   0.73428E+07 0.48600E+00 
c  TempK        0.10101E+05       5   0.34301E-05   0.72620E+01 0.93401E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4976e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.131          19.063       0.0072013      -0.0055174
v  Velocity[Y]             -15.649          15.255         0.22755         0.32578
v  Velocity[Z]             -25.511          11.948         -1.6467        -0.50707
v  ǁVelocityǁ         0.00033666          25.677          7.6964          6.6322
v  Pressure                -513.97          207.06           30.63           34.92
v  k                   9.8686e-011          7.8536         0.21559          0.4593
v  omega                     57.48      2.732e+008     1.2912e+006           76888
v  TempK                    298.57          363.17          336.95          345.08
v  TurbVisc             2.473e-018        0.001903     5.3418e-005      0.00018861
v  CourantNb            0.00019564           1.539         0.79183         0.97369
v  FourierNb             0.0038083               1         0.41271          0.1665
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034511     7.3929e-005      0.00020169

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.41          306.51
v  Yplus               0           2.921         0.63098         0.48716


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67208          2.1332          1.2045          1.1402


 INSTANT    0.729000000E-02   TIME STEP NUMBER             729
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924108E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12802E-01 0.46700E+01
   Friction velocity        uk    :  0.12802E-01 0.46660E+01
   Dimensionless distance   yplus :  0.86797E-02 0.29211E+01
   Friction thermal sca.    tstar :  0.12141E+01 0.19430E+03
   Rough dim-less th. sca.  tplus :  0.61488E-02 0.20693E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27506E+00      10   0.13274E-04   0.42686E+01 0.32338E+02 
c  Velocity[X]                                      0.16898E+01 
c  Velocity[Y]                                      0.11887E+01 
c  Velocity[Z]                                      0.13901E+01 
c  Pressure     0.15894E-04      18   0.27248E-03   0.15930E-01 0.14878E+02 
c  k            0.18070E-01      12   0.92906E-04   0.16644E+00 0.62946E+02 
c  omega        0.27922E+07       1   0.86355E-07   0.10619E+08 0.55741E+00 
c  TempK        0.10101E+05       5   0.34255E-05   0.72626E+01 0.93358E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4953e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.129          19.064       0.0071718      -0.0054673
v  Velocity[Y]             -15.581          15.259         0.22807         0.32641
v  Velocity[Z]             -25.513          11.948         -1.6466        -0.50705
v  ǁVelocityǁ         0.00033328          25.679           7.696          6.6311
v  Pressure                -514.21          207.12          30.697          34.996
v  k                   9.8682e-011          7.8568         0.21586         0.45991
v  omega                     57.48      2.732e+008     1.2912e+006           76888
v  TempK                    298.57          363.17          336.96          345.09
v  TurbVisc            2.4729e-018       0.0019181     5.3496e-005      0.00018885
v  CourantNb            0.00019623          1.5396          0.7918         0.97366
v  FourierNb             0.0038087               1         0.41278          0.1667
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.003472     7.3932e-005      0.00020173

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.41          306.51
v  Yplus               0          2.9211         0.63095         0.48712


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62936          2.1338          1.2046          1.1404


 INSTANT    0.730000000E-02   TIME STEP NUMBER             730
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924167E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12218E-01 0.46699E+01
   Friction velocity        uk    :  0.12218E-01 0.46659E+01
   Dimensionless distance   yplus :  0.82842E-02 0.29212E+01
   Friction thermal sca.    tstar :  0.12141E+01 0.20358E+03
   Rough dim-less th. sca.  tplus :  0.58686E-02 0.20694E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27503E+00      10   0.13160E-04   0.42767E+01 0.32359E+02 
c  Velocity[X]                                      0.16950E+01 
c  Velocity[Y]                                      0.11927E+01 
c  Velocity[Z]                                      0.13889E+01 
c  Pressure     0.15891E-04      18   0.27303E-03   0.15930E-01 0.15062E+02 
c  k            0.18092E-01      12   0.90517E-04   0.16411E+00 0.62406E+02 
c  omega        0.27922E+07       1   0.85066E-07   0.62143E+07 0.46355E+00 
c  TempK        0.10100E+05       5   0.34207E-05   0.72652E+01 0.93312E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4926e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.127          19.064       0.0071429      -0.0054156
v  Velocity[Y]             -15.563          15.263         0.22859         0.32705
v  Velocity[Z]             -25.516          11.947         -1.6466        -0.50703
v  ǁVelocityǁ         0.00033042          25.682          7.6955          6.6301
v  Pressure                -514.47          207.19          30.766          35.072
v  k                   9.8677e-011          7.8553         0.21613         0.46052
v  omega                     57.48      2.732e+008     1.2912e+006           76887
v  TempK                    298.57          363.17          336.97          345.11
v  TurbVisc            2.4728e-018       0.0019321     5.3575e-005      0.00018909
v  CourantNb            0.00019677          1.5402         0.79177         0.97362
v  FourierNb              0.003809               1         0.41286         0.16689
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036496     7.3936e-005      0.00020176

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.41          306.51
v  Yplus               0          2.9212         0.63091         0.48708


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41619          2.1344          1.2046          1.1405


 INSTANT    0.731000000E-02   TIME STEP NUMBER             731
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924145E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11669E-01 0.46698E+01
   Friction velocity        uk    :  0.11669E-01 0.46658E+01
   Dimensionless distance   yplus :  0.79116E-02 0.29213E+01
   Friction thermal sca.    tstar :  0.12141E+01 0.27157E+03
   Rough dim-less th. sca.  tplus :  0.56046E-02 0.20695E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27500E+00      10   0.13079E-04   0.42956E+01 0.32410E+02 
c  Velocity[X]                                      0.17006E+01 
c  Velocity[Y]                                      0.11968E+01 
c  Velocity[Z]                                      0.13981E+01 
c  Pressure     0.16186E-04      18   0.27937E-03   0.16229E-01 0.15692E+02 
c  k            0.18114E-01      12   0.87881E-04   0.16164E+00 0.61851E+02 
c  omega        0.27922E+07       1   0.86610E-07   0.84609E+07 0.51657E+00 
c  TempK        0.10100E+05       5   0.34155E-05   0.72638E+01 0.93266E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4896e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.124          19.065        0.007117      -0.0053612
v  Velocity[Y]             -15.576          15.268         0.22912          0.3277
v  Velocity[Z]             -25.518          11.946         -1.6465        -0.50701
v  ǁVelocityǁ         0.00032841          25.684           7.695           6.629
v  Pressure                -514.74          207.25          30.839          35.152
v  k                   9.8673e-011          7.8565          0.2164         0.46112
v  omega                     57.48      2.732e+008     1.2912e+006           76887
v  TempK                    298.57          363.17          336.98          345.12
v  TurbVisc            2.4727e-018       0.0019451     5.3654e-005      0.00018933
v  CourantNb            0.00019736          1.5409         0.79175         0.97359
v  FourierNb             0.0038093               1         0.41293         0.16709
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036181     7.3939e-005       0.0002018

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.42          306.51
v  Yplus               0          2.9213         0.63088         0.48705


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64127          2.1352          1.2047          1.1407


 INSTANT    0.732000000E-02   TIME STEP NUMBER             732
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924130E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11251E-01 0.46696E+01
   Friction velocity        uk    :  0.11251E-01 0.46657E+01
   Dimensionless distance   yplus :  0.76281E-02 0.29213E+01
   Friction thermal sca.    tstar :  0.12141E+01 0.22109E+03
   Rough dim-less th. sca.  tplus :  0.54038E-02 0.20695E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27497E+00      10   0.12896E-04   0.42993E+01 0.32469E+02 
c  Velocity[X]                                      0.17074E+01 
c  Velocity[Y]                                      0.12027E+01 
c  Velocity[Z]                                      0.13892E+01 
c  Pressure     0.15904E-04      18   0.27682E-03   0.15948E-01 0.15887E+02 
c  k            0.18136E-01      12   0.84739E-04   0.15894E+00 0.61265E+02 
c  omega        0.27922E+07       1   0.90243E-07   0.17673E+08 0.68691E+00 
c  TempK        0.10099E+05       5   0.34122E-05   0.72566E+01 0.93208E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4862e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.122          19.065       0.0070948      -0.0052997
v  Velocity[Y]              -15.67          15.272         0.22964         0.32836
v  Velocity[Z]              -25.52          11.944         -1.6465        -0.50698
v  ǁVelocityǁ         0.00032137          25.686          7.6945           6.628
v  Pressure                -515.01          207.32          30.914          35.236
v  k                   9.8669e-011          7.8447         0.21666         0.46173
v  omega                     57.48      2.732e+008     1.2912e+006           76887
v  TempK                    298.57          363.17          336.99          345.14
v  TurbVisc            2.4726e-018       0.0019571     5.3732e-005      0.00018957
v  CourantNb            0.00019793          1.5417         0.79172         0.97356
v  FourierNb             0.0038096               1           0.413         0.16729
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035639     7.3942e-005      0.00020183

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.42          306.51
v  Yplus               0          2.9213         0.63085         0.48701


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57923           2.136          1.2047          1.1408


 INSTANT    0.733000000E-02   TIME STEP NUMBER             733
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924145E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10990E-01 0.46695E+01
   Friction velocity        uk    :  0.10989E-01 0.46656E+01
   Dimensionless distance   yplus :  0.74511E-02 0.29214E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.22634E+03
   Rough dim-less th. sca.  tplus :  0.52784E-02 0.20695E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27494E+00      10   0.12825E-04   0.43046E+01 0.32481E+02 
c  Velocity[X]                                      0.17119E+01 
c  Velocity[Y]                                      0.12047E+01 
c  Velocity[Z]                                      0.13880E+01 
c  Pressure     0.15999E-04      18   0.27763E-03   0.16047E-01 0.14800E+02 
c  k            0.18158E-01      12   0.81055E-04   0.15556E+00 0.60625E+02 
c  omega        0.27922E+07       1   0.92695E-07   0.24024E+08 0.78200E+00 
c  TempK        0.10099E+05       5   0.34086E-05   0.72537E+01 0.93155E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4829e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.12          19.066       0.0070706      -0.0052397
v  Velocity[Y]             -15.719          15.275         0.23015         0.32901
v  Velocity[Z]             -25.522          11.942         -1.6464        -0.50696
v  ǁVelocityǁ         0.00029269          25.688           7.694           6.627
v  Pressure                -515.29          207.38          30.981           35.31
v  k                   9.8665e-011           7.825         0.21693         0.46233
v  omega                     57.48      2.732e+008     1.2912e+006           76887
v  TempK                    298.57          363.17             337          345.16
v  TurbVisc            2.4725e-018       0.0019648     5.3811e-005      0.00018981
v  CourantNb            0.00019848          1.5425          0.7917         0.97353
v  FourierNb             0.0038099               1         0.41308         0.16748
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035735     7.3945e-005      0.00020186

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.42          306.51
v  Yplus               0          2.9214         0.63082         0.48697


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65325          2.1368          1.2048           1.141


 INSTANT    0.734000000E-02   TIME STEP NUMBER             734
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924084E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10905E-01 0.46694E+01
   Friction velocity        uk    :  0.10905E-01 0.46655E+01
   Dimensionless distance   yplus :  0.73936E-02 0.29214E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.22810E+03
   Rough dim-less th. sca.  tplus :  0.52377E-02 0.20696E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27491E+00      10   0.13253E-04   0.43099E+01 0.32503E+02 
c  Velocity[X]                                      0.17136E+01 
c  Velocity[Y]                                      0.12093E+01 
c  Velocity[Z]                                      0.13870E+01 
c  Pressure     0.15997E-04      18   0.27668E-03   0.16048E-01 0.14547E+02 
c  k            0.18181E-01      12   0.77793E-04   0.15251E+00 0.60013E+02 
c  omega        0.27922E+07       1   0.89131E-07   0.14873E+08 0.63861E+00 
c  TempK        0.10098E+05       5   0.34039E-05   0.72448E+01 0.93086E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4803e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.118          19.067       0.0070456      -0.0051796
v  Velocity[Y]             -15.642          15.279         0.23067         0.32967
v  Velocity[Z]             -25.524          11.942         -1.6463        -0.50694
v  ǁVelocityǁ         0.00026908           25.69          7.6935          6.6259
v  Pressure                 -515.6          207.45          31.046          35.383
v  k                   9.8661e-011          7.8008         0.21719         0.46294
v  omega                     57.48      2.732e+008     1.2912e+006           76886
v  TempK                    298.56          363.17          337.01          345.17
v  TurbVisc            2.4724e-018       0.0019712     5.3889e-005      0.00019005
v  CourantNb            0.00019898          1.5431         0.79167          0.9735
v  FourierNb             0.0038102               1         0.41315         0.16767
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034642     7.3948e-005      0.00020189

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.42          306.51
v  Yplus               0          2.9214         0.63078         0.48693


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48156          2.1374          1.2048          1.1412


 INSTANT    0.735000000E-02   TIME STEP NUMBER             735
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924044E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11012E-01 0.46693E+01
   Friction velocity        uk    :  0.11012E-01 0.46654E+01
   Dimensionless distance   yplus :  0.74665E-02 0.29215E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.22588E+03
   Rough dim-less th. sca.  tplus :  0.52893E-02 0.20696E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27489E+00      10   0.13416E-04   0.43101E+01 0.32467E+02 
c  Velocity[X]                                      0.17162E+01 
c  Velocity[Y]                                      0.12065E+01 
c  Velocity[Z]                                      0.13874E+01 
c  Pressure     0.16095E-04      18   0.28014E-03   0.16150E-01 0.13852E+02 
c  k            0.18204E-01      12   0.74639E-04   0.15042E+00 0.59479E+02 
c  omega        0.27922E+07       1   0.86039E-07   0.65926E+07 0.47099E+00 
c  TempK        0.10098E+05       5   0.34012E-05   0.72341E+01 0.93025E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4779e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.116          19.067       0.0070206      -0.0051204
v  Velocity[Y]             -15.584          15.283         0.23119         0.33033
v  Velocity[Z]             -25.526          11.941         -1.6463        -0.50691
v  ǁVelocityǁ         0.00025188          25.692          7.6931          6.6249
v  Pressure                -515.93           207.5          31.105           35.45
v  k                   9.8657e-011          7.7735         0.21745         0.46354
v  omega                     57.48      2.732e+008     1.2912e+006           76886
v  TempK                    298.56          363.17          337.02          345.19
v  TurbVisc            2.4723e-018        0.001977     5.3968e-005       0.0001903
v  CourantNb            0.00019956          1.5437         0.79164         0.97346
v  FourierNb             0.0038104               1         0.41322         0.16787
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035232     7.3951e-005      0.00020192

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.42          306.51
v  Yplus               0          2.9215         0.63075         0.48689


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49551           2.138          1.2049          1.1413


 INSTANT    0.736000000E-02   TIME STEP NUMBER             736
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924054E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11272E-01 0.46692E+01
   Friction velocity        uk    :  0.11272E-01 0.46653E+01
   Dimensionless distance   yplus :  0.76424E-02 0.29216E+01
   Friction thermal sca.    tstar :  0.12139E+01 0.22068E+03
   Rough dim-less th. sca.  tplus :  0.54139E-02 0.20697E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27486E+00      10   0.13282E-04   0.43181E+01 0.32493E+02 
c  Velocity[X]                                      0.17199E+01 
c  Velocity[Y]                                      0.12101E+01 
c  Velocity[Z]                                      0.13880E+01 
c  Pressure     0.16006E-04      18   0.27985E-03   0.16064E-01 0.13842E+02 
c  k            0.18226E-01      12   0.72164E-04   0.14863E+00 0.58976E+02 
c  omega        0.27922E+07       1   0.85761E-07   0.62306E+07 0.46087E+00 
c  TempK        0.10097E+05       5   0.33981E-05   0.72227E+01 0.92968E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4751e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.114          19.068       0.0069951      -0.0050629
v  Velocity[Y]             -15.576          15.287         0.23171           0.331
v  Velocity[Z]             -25.529          11.939         -1.6462        -0.50689
v  ǁVelocityǁ         0.00024203          25.694          7.6926          6.6239
v  Pressure                -516.27          207.55          31.164          35.518
v  k                   9.8653e-011           7.745         0.21771         0.46415
v  omega                     57.48      2.732e+008     1.2912e+006           76886
v  TempK                    298.56          363.17          337.02           345.2
v  TurbVisc            2.4722e-018       0.0019821     5.4046e-005      0.00019054
v  CourantNb            0.00013876          1.5444         0.79162         0.97343
v  FourierNb             0.0038107               1         0.41329         0.16806
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035663     7.3954e-005      0.00020195

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.42          306.52
v  Yplus               0          2.9216         0.63072         0.48685


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52445          2.1386          1.2049          1.1415


 INSTANT    0.737000000E-02   TIME STEP NUMBER             737
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924102E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11680E-01 0.46691E+01
   Friction velocity        uk    :  0.11680E-01 0.46652E+01
   Dimensionless distance   yplus :  0.79194E-02 0.29216E+01
   Friction thermal sca.    tstar :  0.12141E+01 0.21296E+03
   Rough dim-less th. sca.  tplus :  0.56101E-02 0.20697E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27483E+00      10   0.12987E-04   0.43249E+01 0.32524E+02 
c  Velocity[X]                                      0.17239E+01 
c  Velocity[Y]                                      0.12123E+01 
c  Velocity[Z]                                      0.13887E+01 
c  Pressure     0.16187E-04      17   0.28096E-03   0.16249E-01 0.13374E+02 
c  k            0.18249E-01      12   0.70118E-04   0.14668E+00 0.58456E+02 
c  omega        0.27922E+07       1   0.85622E-07   0.60696E+07 0.45434E+00 
c  TempK        0.10097E+05       5   0.33950E-05   0.72094E+01 0.92914E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4721e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.112          19.069       0.0069729      -0.0050032
v  Velocity[Y]             -15.596          15.291         0.23222         0.33168
v  Velocity[Z]             -25.531          11.938         -1.6462        -0.50687
v  ǁVelocityǁ         0.00024011          25.696          7.6922          6.6228
v  Pressure                -516.62           207.6           31.22          35.581
v  k                   9.8649e-011          7.7167         0.21797         0.46475
v  omega                     57.48      2.732e+008     1.2912e+006           76886
v  TempK                    298.56          363.17          337.03          345.22
v  TurbVisc            2.4721e-018       0.0019866     5.4123e-005      0.00019078
v  CourantNb            0.00012042          1.5451         0.79159          0.9734
v  FourierNb              0.003811               1         0.41336         0.16825
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035595     7.3956e-005      0.00020198

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.42          306.52
v  Yplus               0          2.9216         0.63069         0.48682


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59435          2.1394           1.205          1.1416


 INSTANT    0.738000000E-02   TIME STEP NUMBER             738
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923970E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12147E-01 0.46690E+01
   Friction velocity        uk    :  0.12147E-01 0.46651E+01
   Dimensionless distance   yplus :  0.82360E-02 0.29217E+01
   Friction thermal sca.    tstar :  0.12141E+01 0.20478E+03
   Rough dim-less th. sca.  tplus :  0.58344E-02 0.20697E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27480E+00      10   0.12831E-04   0.43392E+01 0.32582E+02 
c  Velocity[X]                                      0.17289E+01 
c  Velocity[Y]                                      0.12143E+01 
c  Velocity[Z]                                      0.13960E+01 
c  Pressure     0.16554E-04      17   0.28465E-03   0.16622E-01 0.14101E+02 
c  k            0.18272E-01      12   0.68039E-04   0.14443E+00 0.57920E+02 
c  omega        0.27922E+07       1   0.90455E-07   0.15364E+08 0.63457E+00 
c  TempK        0.10096E+05       5   0.33913E-05   0.71948E+01 0.92876E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4688e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.11          19.069       0.0069508      -0.0049434
v  Velocity[Y]             -15.725          15.295         0.23273         0.33235
v  Velocity[Z]             -25.533          11.937         -1.6461        -0.50685
v  ǁVelocityǁ         0.00024586          25.699          7.6917          6.6218
v  Pressure                -516.97          207.65          31.281           35.65
v  k                   9.8646e-011          7.7205         0.21823         0.46535
v  omega                     57.48      2.732e+008     1.2912e+006           76885
v  TempK                    298.56          363.17          337.04          345.23
v  TurbVisc             2.472e-018       0.0019907     5.4201e-005      0.00019102
v  CourantNb            0.00012258          1.5459         0.79157         0.97336
v  FourierNb             0.0038112               1         0.41343         0.16843
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035889     7.3956e-005      0.00020201

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.42          306.52
v  Yplus               0          2.9217         0.63067         0.48678


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49536          2.1402           1.205          1.1418


 INSTANT    0.739000000E-02   TIME STEP NUMBER             739
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923962E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12665E-01 0.46689E+01
   Friction velocity        uk    :  0.12665E-01 0.46650E+01
   Dimensionless distance   yplus :  0.85868E-02 0.29218E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.19641E+03
   Rough dim-less th. sca.  tplus :  0.60830E-02 0.20698E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27477E+00      10   0.12909E-04   0.43542E+01 0.32659E+02 
c  Velocity[X]                                      0.17340E+01 
c  Velocity[Y]                                      0.12192E+01 
c  Velocity[Z]                                      0.14010E+01 
c  Pressure     0.16163E-04      18   0.28159E-03   0.16233E-01 0.13705E+02 
c  k            0.18294E-01      12   0.65623E-04   0.14152E+00 0.57346E+02 
c  omega        0.27922E+07       1   0.88793E-07   0.13239E+08 0.59902E+00 
c  TempK        0.10096E+05       5   0.33865E-05   0.71845E+01 0.92805E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4659e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.107           19.07       0.0069323      -0.0048856
v  Velocity[Y]             -15.701          15.299         0.23324         0.33304
v  Velocity[Z]             -25.536          11.936         -1.6461        -0.50683
v  ǁVelocityǁ         0.00025826          25.701          7.6913          6.6208
v  Pressure                -517.33           207.7          31.339          35.716
v  k                   9.8642e-011          7.7401         0.21848         0.46596
v  omega                     57.48      2.732e+008     1.2912e+006           76885
v  TempK                    298.56          363.17          337.05          345.25
v  TurbVisc            2.4719e-018       0.0019954     5.4278e-005      0.00019126
v  CourantNb            0.00018806          1.5466         0.79154         0.97333
v  FourierNb             0.0038114               1          0.4135         0.16862
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037721     7.3957e-005      0.00020203

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.42          306.52
v  Yplus               0          2.9218         0.63064         0.48674


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59701          2.1409           1.205          1.1419


 INSTANT    0.740000000E-02   TIME STEP NUMBER             740
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924100E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13199E-01 0.46688E+01
   Friction velocity        uk    :  0.13199E-01 0.46649E+01
   Dimensionless distance   yplus :  0.89493E-02 0.29219E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.18845E+03
   Rough dim-less th. sca.  tplus :  0.63398E-02 0.20699E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27474E+00      10   0.12928E-04   0.43424E+01 0.32646E+02 
c  Velocity[X]                                      0.17374E+01 
c  Velocity[Y]                                      0.12162E+01 
c  Velocity[Z]                                      0.13888E+01 
c  Pressure     0.15939E-04      17   0.28349E-03   0.16012E-01 0.13314E+02 
c  k            0.18317E-01      12   0.63766E-04   0.13886E+00 0.56786E+02 
c  omega        0.27922E+07       1   0.86424E-07   0.74705E+07 0.48422E+00 
c  TempK        0.10096E+05       5   0.33815E-05   0.71760E+01 0.92749E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4636e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.105          19.071       0.0069111      -0.0048311
v  Velocity[Y]             -15.639          15.302         0.23375         0.33372
v  Velocity[Z]             -25.538          11.934          -1.646        -0.50681
v  ǁVelocityǁ         0.00027621          25.703          7.6909          6.6198
v  Pressure                -517.71          207.75          31.394          35.779
v  k                   9.8638e-011          7.7574         0.21874         0.46657
v  omega                     57.48      2.732e+008     1.2912e+006           76885
v  TempK                    298.55          363.17          337.06          345.27
v  TurbVisc            2.4718e-018       0.0020036     5.4355e-005       0.0001915
v  CourantNb             0.0002021          1.5471         0.79152         0.97329
v  FourierNb             0.0038116               1         0.41356          0.1688
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038112     7.3958e-005      0.00020206

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.42          306.52
v  Yplus               0          2.9219         0.63061         0.48671


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63007          2.1414          1.2051          1.1421


 INSTANT    0.741000000E-02   TIME STEP NUMBER             741
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924109E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13730E-01 0.46688E+01
   Friction velocity        uk    :  0.13730E-01 0.46648E+01
   Dimensionless distance   yplus :  0.93089E-02 0.29219E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.18405E+03
   Rough dim-less th. sca.  tplus :  0.65945E-02 0.20699E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27472E+00      10   0.12832E-04   0.43481E+01 0.32681E+02 
c  Velocity[X]                                      0.17414E+01 
c  Velocity[Y]                                      0.12137E+01 
c  Velocity[Z]                                      0.13930E+01 
c  Pressure     0.16115E-04      17   0.28758E-03   0.16194E-01 0.13264E+02 
c  k            0.18341E-01      12   0.62189E-04   0.13644E+00 0.56257E+02 
c  omega        0.27922E+07       1   0.88293E-07   0.12394E+08 0.58496E+00 
c  TempK        0.10095E+05       5   0.33762E-05   0.71625E+01 0.92704E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4614e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.103          19.071       0.0068852      -0.0047805
v  Velocity[Y]             -15.572          15.306         0.23427         0.33441
v  Velocity[Z]             -25.541          11.932          -1.646         -0.5068
v  ǁVelocityǁ         0.00029863          25.706          7.6904          6.6188
v  Pressure                -518.11           207.8          31.447           35.84
v  k                   9.8634e-011          7.7726         0.21899         0.46719
v  omega                    57.481     2.7319e+008     1.2912e+006           76885
v  TempK                    298.55          363.17          337.07          345.28
v  TurbVisc            2.4717e-018       0.0020115     5.4431e-005      0.00019175
v  CourantNb            0.00020261          1.5476         0.79149         0.97326
v  FourierNb             0.0038118               1         0.41363         0.16899
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038467     7.3959e-005      0.00020209

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.42          306.52
v  Yplus               0          2.9219         0.63059         0.48667


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42041           2.142          1.2051          1.1423


 INSTANT    0.742000000E-02   TIME STEP NUMBER             742
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923937E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13737E-01 0.46687E+01
   Friction velocity        uk    :  0.13737E-01 0.46647E+01
   Dimensionless distance   yplus :  0.93138E-02 0.29220E+01
   Friction thermal sca.    tstar :  0.12141E+01 0.18395E+03
   Rough dim-less th. sca.  tplus :  0.65980E-02 0.20700E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27469E+00      10   0.12818E-04   0.43515E+01 0.32741E+02 
c  Velocity[X]                                      0.17460E+01 
c  Velocity[Y]                                      0.12162E+01 
c  Velocity[Z]                                      0.13892E+01 
c  Pressure     0.15894E-04      18   0.28524E-03   0.15975E-01 0.14062E+02 
c  k            0.18364E-01      12   0.61517E-04   0.13435E+00 0.55769E+02 
c  omega        0.27922E+07       1   0.88975E-07   0.13806E+08 0.61375E+00 
c  TempK        0.10095E+05       5   0.33709E-05   0.71424E+01 0.92652E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4589e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.101          19.072       0.0068592      -0.0047324
v  Velocity[Y]             -15.553           15.31         0.23479         0.33511
v  Velocity[Z]             -25.543          11.929         -1.6459        -0.50679
v  ǁVelocityǁ         0.00032428          25.708            7.69          6.6178
v  Pressure                -518.51          207.85          31.508          35.909
v  k                   9.8631e-011           7.786         0.21924         0.46781
v  omega                    57.481     2.7319e+008     1.2912e+006           76884
v  TempK                    298.55          363.17          337.08           345.3
v  TurbVisc            2.4716e-018       0.0020191     5.4508e-005        0.000192
v  CourantNb            0.00020312          1.5483         0.79147         0.97322
v  FourierNb              0.003812               1          0.4137         0.16918
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038793      7.396e-005      0.00020211

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.42          306.52
v  Yplus               0           2.922         0.63056         0.48664


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58861          2.1426          1.2052          1.1424


 INSTANT    0.743000000E-02   TIME STEP NUMBER             743
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924219E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13748E-01 0.46686E+01
   Friction velocity        uk    :  0.13748E-01 0.46646E+01
   Dimensionless distance   yplus :  0.93211E-02 0.29220E+01
   Friction thermal sca.    tstar :  0.12141E+01 0.18381E+03
   Rough dim-less th. sca.  tplus :  0.66031E-02 0.20700E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27466E+00      10   0.12773E-04   0.43570E+01 0.32758E+02 
c  Velocity[X]                                      0.17501E+01 
c  Velocity[Y]                                      0.12150E+01 
c  Velocity[Z]                                      0.13920E+01 
c  Pressure     0.16148E-04      18   0.29042E-03   0.16235E-01 0.12704E+02 
c  k            0.18388E-01      12   0.60910E-04   0.13249E+00 0.55319E+02 
c  omega        0.27922E+07       1   0.87530E-07   0.85808E+07 0.51212E+00 
c  TempK        0.10094E+05       5   0.33653E-05   0.71184E+01 0.92582E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4559e-007                             7


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.099          19.073        0.006829      -0.0046852
v  Velocity[Y]             -15.564          15.313         0.23531          0.3358
v  Velocity[Z]             -25.545          11.926         -1.6458        -0.50677
v  ǁVelocityǁ         0.00035195           25.71          7.6896          6.6169
v  Pressure                -518.93          207.89          31.557          35.966
v  k                   9.8627e-011          7.8002          0.2195         0.46842
v  omega                    57.481     2.7319e+008     1.2912e+006           76884
v  TempK                    298.55          363.17          337.09          345.31
v  TurbVisc            2.4715e-018       0.0020264     5.4585e-005      0.00019224
v  CourantNb             0.0002036           1.549         0.79144         0.97319
v  FourierNb             0.0038122               1         0.41376         0.16937
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039088     7.3962e-005      0.00020214

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.42          306.52
v  Yplus               0           2.922         0.63053          0.4866


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42153          2.1433          1.2052          1.1426


 INSTANT    0.744000000E-02   TIME STEP NUMBER             744
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924185E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13754E-01 0.46685E+01
   Friction velocity        uk    :  0.13754E-01 0.46645E+01
   Dimensionless distance   yplus :  0.93253E-02 0.29221E+01
   Friction thermal sca.    tstar :  0.12141E+01 0.18372E+03
   Rough dim-less th. sca.  tplus :  0.66061E-02 0.20700E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27463E+00      10   0.12727E-04   0.43636E+01 0.32793E+02 
c  Velocity[X]                                      0.17546E+01 
c  Velocity[Y]                                      0.12131E+01 
c  Velocity[Z]                                      0.13958E+01 
c  Pressure     0.15999E-04      18   0.29278E-03   0.16090E-01 0.13062E+02 
c  k            0.18412E-01      12   0.60623E-04   0.13084E+00 0.54909E+02 
c  omega        0.27922E+07       1   0.88366E-07   0.91691E+07 0.52543E+00 
c  TempK        0.10094E+05       5   0.33591E-05   0.70939E+01 0.92527E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4527e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.097          19.074       0.0067991      -0.0046425
v  Velocity[Y]             -15.656          15.317         0.23583          0.3365
v  Velocity[Z]             -25.547          11.927         -1.6458        -0.50676
v  ǁVelocityǁ         0.00035834          25.712          7.6892          6.6159
v  Pressure                -519.35          207.94          31.608          36.025
v  k                   9.8623e-011          7.8188         0.21975         0.46905
v  omega                    57.481     2.7319e+008     1.2912e+006           76884
v  TempK                    298.55          363.17           337.1          345.33
v  TurbVisc            2.4714e-018       0.0020334     5.4661e-005      0.00019249
v  CourantNb            0.00020405          1.5497         0.79142         0.97315
v  FourierNb             0.0038123               1         0.41383         0.16956
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0039295     7.3963e-005      0.00020216

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.43          306.52
v  Yplus               0          2.9221          0.6305         0.48656


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65341          2.1441          1.2052          1.1427


 INSTANT    0.745000000E-02   TIME STEP NUMBER             745
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924218E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13756E-01 0.46684E+01
   Friction velocity        uk    :  0.13756E-01 0.46645E+01
   Dimensionless distance   yplus :  0.93268E-02 0.29222E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.18369E+03
   Rough dim-less th. sca.  tplus :  0.66072E-02 0.20701E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27460E+00      10   0.12682E-04   0.43606E+01 0.32846E+02 
c  Velocity[X]                                      0.17585E+01 
c  Velocity[Y]                                      0.12149E+01 
c  Velocity[Z]                                      0.13872E+01 
c  Pressure     0.15848E-04      18   0.29145E-03   0.15942E-01 0.12887E+02 
c  k            0.18435E-01      12   0.60486E-04   0.12945E+00 0.54550E+02 
c  omega        0.27922E+07       1   0.93130E-07   0.21875E+08 0.74821E+00 
c  TempK        0.10093E+05       5   0.33537E-05   0.70695E+01 0.92483E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4495e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.095          19.074       0.0067697      -0.0046045
v  Velocity[Y]             -15.706           15.32         0.23635          0.3372
v  Velocity[Z]             -25.549          11.928         -1.6457        -0.50674
v  ǁVelocityǁ         0.00036367          25.714          7.6888          6.6149
v  Pressure                -519.78          207.98          31.657          36.081
v  k                   9.8619e-011           7.835            0.22         0.46967
v  omega                    57.481     2.7319e+008     1.2912e+006           76884
v  TempK                    298.55          363.17           337.1          345.34
v  TurbVisc            2.4714e-018       0.0020402     5.4738e-005      0.00019274
v  CourantNb            0.00020451          1.5505         0.79139         0.97311
v  FourierNb             0.0038125               1          0.4139         0.16975
v  total_pressure      1.0081e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035929     7.3964e-005      0.00020218

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.43          306.52
v  Yplus               0          2.9222         0.63047         0.48652


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55299          2.1449          1.2053          1.1429


 INSTANT    0.746000000E-02   TIME STEP NUMBER             746
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924111E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13757E-01 0.46683E+01
   Friction velocity        uk    :  0.13757E-01 0.46644E+01
   Dimensionless distance   yplus :  0.93277E-02 0.29222E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.18367E+03
   Rough dim-less th. sca.  tplus :  0.66078E-02 0.20701E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27457E+00      10   0.12698E-04   0.43638E+01 0.32901E+02 
c  Velocity[X]                                      0.17594E+01 
c  Velocity[Y]                                      0.12176E+01 
c  Velocity[Z]                                      0.13868E+01 
c  Pressure     0.15976E-04      18   0.29506E-03   0.16075E-01 0.12839E+02 
c  k            0.18459E-01      12   0.60600E-04   0.12827E+00 0.54242E+02 
c  omega        0.27922E+07       1   0.90883E-07   0.15000E+08 0.64356E+00 
c  TempK        0.10093E+05       5   0.33472E-05   0.70427E+01 0.92419E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4471e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.093          19.075       0.0067369      -0.0045701
v  Velocity[Y]             -15.633          15.324         0.23687          0.3379
v  Velocity[Z]             -25.552          11.928         -1.6456        -0.50672
v  ǁVelocityǁ         0.00036893          25.716          7.6884          6.6139
v  Pressure                -520.23          208.02          31.706          36.138
v  k                   9.8616e-011          7.8488         0.22025          0.4703
v  omega                    57.481     2.7319e+008     1.2912e+006           76883
v  TempK                    298.55          363.17          337.11          345.36
v  TurbVisc            2.4713e-018       0.0020467     5.4815e-005        0.000193
v  CourantNb            0.00020497          1.5511         0.79136         0.97308
v  FourierNb             0.0038126               1         0.41397         0.16994
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035434     7.3965e-005       0.0002022

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.43          306.52
v  Yplus               0          2.9222         0.63045         0.48648


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53447          2.1455          1.2053           1.143


 INSTANT    0.747000000E-02   TIME STEP NUMBER             747
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924106E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13775E-01 0.46682E+01
   Friction velocity        uk    :  0.13775E-01 0.46643E+01
   Dimensionless distance   yplus :  0.93398E-02 0.29223E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.18344E+03
   Rough dim-less th. sca.  tplus :  0.66164E-02 0.20702E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27454E+00      10   0.12751E-04   0.43562E+01 0.32872E+02 
c  Velocity[X]                                      0.17594E+01 
c  Velocity[Y]                                      0.12109E+01 
c  Velocity[Z]                                      0.13858E+01 
c  Pressure     0.16075E-04      18   0.29711E-03   0.16179E-01 0.12624E+02 
c  k            0.18483E-01      12   0.60822E-04   0.12725E+00 0.53975E+02 
c  omega        0.27922E+07       1   0.88601E-07   0.72432E+07 0.49717E+00 
c  TempK        0.10093E+05       5   0.33406E-05   0.70197E+01 0.92375E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4448e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.091          19.076       0.0067057      -0.0045393
v  Velocity[Y]             -15.575          15.327          0.2374          0.3386
v  Velocity[Z]             -25.554          11.927         -1.6456        -0.50671
v  ǁVelocityǁ         0.00037437          25.719           7.688           6.613
v  Pressure                -520.68          208.06          31.752          36.192
v  k                   9.8612e-011          7.8604         0.22049         0.47092
v  omega                    57.481     2.7319e+008     1.2912e+006           76883
v  TempK                    298.55          363.17          337.12          345.37
v  TurbVisc            2.4712e-018       0.0020529     5.4892e-005      0.00019326
v  CourantNb            0.00020539          1.5516         0.79134         0.97304
v  FourierNb             0.0038128               1         0.41404         0.17014
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035546     7.3966e-005      0.00020223

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.43          306.52
v  Yplus               0          2.9223         0.63042         0.48645


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58726           2.146          1.2054          1.1432


 INSTANT    0.748000000E-02   TIME STEP NUMBER             748
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924094E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13793E-01 0.46682E+01
   Friction velocity        uk    :  0.13793E-01 0.46642E+01
   Dimensionless distance   yplus :  0.93518E-02 0.29224E+01
   Friction thermal sca.    tstar :  0.12140E+01 0.18320E+03
   Rough dim-less th. sca.  tplus :  0.66248E-02 0.20702E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27452E+00      10   0.12739E-04   0.43618E+01 0.32904E+02 
c  Velocity[X]                                      0.17616E+01 
c  Velocity[Y]                                      0.12106E+01 
c  Velocity[Z]                                      0.13896E+01 
c  Pressure     0.16255E-04      17   0.29818E-03   0.16364E-01 0.12296E+02 
c  k            0.18507E-01      12   0.61881E-04   0.12636E+00 0.53747E+02 
c  omega        0.27922E+07       1   0.88994E-07   0.72553E+07 0.50409E+00 
c  TempK        0.10092E+05       5   0.33336E-05   0.69986E+01 0.92331E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4423e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.089          19.076       0.0066726      -0.0045125
v  Velocity[Y]             -15.566          15.331         0.23792         0.33931
v  Velocity[Z]             -25.557          11.925         -1.6455        -0.50669
v  ǁVelocityǁ         0.00038013          25.721          7.6876           6.612
v  Pressure                -521.14           208.1          31.795          36.244
v  k                   9.8608e-011          7.8698         0.22074         0.47155
v  omega                    57.481     2.7319e+008     1.2912e+006           76883
v  TempK                    298.55          363.17          337.13          345.39
v  TurbVisc            2.4711e-018       0.0020589      5.497e-005      0.00019351
v  CourantNb             0.0002058          1.5522         0.79131           0.973
v  FourierNb             0.0038129               1         0.41411         0.17033
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035651     7.3967e-005      0.00020225

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.43          306.52
v  Yplus               0          2.9224         0.63039         0.48641


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.3871          2.1467          1.2054          1.1433


 INSTANT    0.749000000E-02   TIME STEP NUMBER             749
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923917E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13802E-01 0.46681E+01
   Friction velocity        uk    :  0.13802E-01 0.46641E+01
   Dimensionless distance   yplus :  0.93579E-02 0.29225E+01
   Friction thermal sca.    tstar :  0.12141E+01 0.18308E+03
   Rough dim-less th. sca.  tplus :  0.66292E-02 0.20703E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27449E+00      10   0.12817E-04   0.43688E+01 0.32943E+02 
c  Velocity[X]                                      0.17636E+01 
c  Velocity[Y]                                      0.12102E+01 
c  Velocity[Z]                                      0.13950E+01 
c  Pressure     0.16635E-04      17   0.29906E-03   0.16751E-01 0.12621E+02 
c  k            0.18531E-01      12   0.62596E-04   0.12564E+00 0.53561E+02 
c  omega        0.27922E+07       1   0.89234E-07   0.71583E+07 0.50598E+00 
c  TempK        0.10092E+05       5   0.33256E-05   0.69744E+01 0.92274E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4394e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.088          19.077       0.0066391      -0.0044916
v  Velocity[Y]             -15.584          15.334         0.23845         0.34002
v  Velocity[Z]             -25.559          11.922         -1.6454        -0.50668
v  ǁVelocityǁ         0.00038572          25.723          7.6872           6.611
v  Pressure                -521.61          208.14          31.841          36.297
v  k                   9.8605e-011          7.8771         0.22099         0.47218
v  omega                    57.482     2.7319e+008     1.2912e+006           76883
v  TempK                    298.55          363.17          337.14           345.4
v  TurbVisc             2.471e-018        0.002065     5.5047e-005      0.00019377
v  CourantNb            0.00020621          1.5529         0.79129         0.97296
v  FourierNb              0.003813               1         0.41417         0.17052
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035749     7.3967e-005      0.00020227

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.43          306.52
v  Yplus               0          2.9225         0.63036         0.48637


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57328          2.1474          1.2055          1.1435


 INSTANT    0.750000000E-02   TIME STEP NUMBER             750
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923889E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13814E-01 0.46680E+01
   Friction velocity        uk    :  0.13814E-01 0.46641E+01
   Dimensionless distance   yplus :  0.93661E-02 0.29225E+01
   Friction thermal sca.    tstar :  0.12142E+01 0.18292E+03
   Rough dim-less th. sca.  tplus :  0.66350E-02 0.20704E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27446E+00      10   0.12837E-04   0.43606E+01 0.32992E+02 
c  Velocity[X]                                      0.17657E+01 
c  Velocity[Y]                                      0.12096E+01 
c  Velocity[Z]                                      0.13853E+01 
c  Pressure     0.16288E-04      18   0.29980E-03   0.16405E-01 0.13630E+02 
c  k            0.18555E-01      12   0.63140E-04   0.12510E+00 0.53436E+02 
c  omega        0.27922E+07       1   0.94912E-07   0.18252E+08 0.70445E+00 
c  TempK        0.10091E+05       5   0.33177E-05   0.69512E+01 0.92241E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4362e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.086          19.078        0.006602      -0.0044748
v  Velocity[Y]             -15.713          15.337         0.23897         0.34073
v  Velocity[Z]             -25.562          11.918         -1.6453        -0.50667
v  ǁVelocityǁ         0.00039144          25.726          7.6868          6.6101
v  Pressure                -522.08          208.19          31.896          36.359
v  k                   9.8601e-011           7.886         0.22123         0.47281
v  omega                    57.482     2.7319e+008     1.2912e+006           76882
v  TempK                    298.55          363.17          337.15          345.42
v  TurbVisc            2.4709e-018       0.0020712     5.5123e-005      0.00019403
v  CourantNb            0.00020659          1.5537         0.79126         0.97292
v  FourierNb             0.0038131               1         0.41424         0.17071
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035841     7.3968e-005      0.00020229

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.43          306.53
v  Yplus               0          2.9225         0.63034         0.48634


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6226          2.1481          1.2055          1.1436


 INSTANT    0.751000000E-02   TIME STEP NUMBER             751
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924172E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13817E-01 0.46679E+01
   Friction velocity        uk    :  0.13817E-01 0.46640E+01
   Dimensionless distance   yplus :  0.93679E-02 0.29226E+01
   Friction thermal sca.    tstar :  0.12146E+01 0.18289E+03
   Rough dim-less th. sca.  tplus :  0.66363E-02 0.20704E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27443E+00      10   0.12750E-04   0.43674E+01 0.33088E+02 
c  Velocity[X]                                      0.17687E+01 
c  Velocity[Y]                                      0.12166E+01 
c  Velocity[Z]                                      0.13821E+01 
c  Pressure     0.16454E-04      18   0.30639E-03   0.16575E-01 0.12730E+02 
c  k            0.18579E-01      12   0.64033E-04   0.12473E+00 0.53360E+02 
c  omega        0.27922E+07       1   0.93985E-07   0.17567E+08 0.69962E+00 
c  TempK        0.10091E+05       5   0.33084E-05   0.69254E+01 0.92161E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4335e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.084          19.079       0.0065654      -0.0044648
v  Velocity[Y]             -15.691           15.34         0.23951         0.34144
v  Velocity[Z]             -25.564          11.914         -1.6453        -0.50666
v  ǁVelocityǁ          0.0003972          25.728          7.6864          6.6091
v  Pressure                -522.57          208.24          31.942          36.413
v  k                   9.8597e-011          7.8937         0.22147         0.47344
v  omega                    57.482     2.7319e+008     1.2912e+006           76882
v  TempK                    298.55          363.17          337.16          345.43
v  TurbVisc            2.4708e-018       0.0020774       5.52e-005      0.00019429
v  CourantNb            0.00020696          1.5544         0.79124         0.97288
v  FourierNb             0.0038132               1         0.41431         0.17091
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035927     7.3969e-005      0.00020231

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.43          306.53
v  Yplus               0          2.9226         0.63031          0.4863


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48082          2.1488          1.2055          1.1438


 INSTANT    0.752000000E-02   TIME STEP NUMBER             752
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924007E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13827E-01 0.46679E+01
   Friction velocity        uk    :  0.13827E-01 0.46639E+01
   Dimensionless distance   yplus :  0.93751E-02 0.29226E+01
   Friction thermal sca.    tstar :  0.12146E+01 0.18275E+03
   Rough dim-less th. sca.  tplus :  0.66413E-02 0.20704E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27440E+00      10   0.12667E-04   0.43591E+01 0.33064E+02 
c  Velocity[X]                                      0.17695E+01 
c  Velocity[Y]                                      0.12114E+01 
c  Velocity[Z]                                      0.13782E+01 
c  Pressure     0.16378E-04      18   0.29841E-03   0.16502E-01 0.12143E+02 
c  k            0.18602E-01      12   0.65007E-04   0.12441E+00 0.53305E+02 
c  omega        0.27922E+07       1   0.92623E-07   0.13215E+08 0.63267E+00 
c  TempK        0.10091E+05       5   0.32990E-05   0.69010E+01 0.92084E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4314e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.082          19.079       0.0065252      -0.0044619
v  Velocity[Y]             -15.627          15.343         0.24004         0.34216
v  Velocity[Z]             -25.566          11.909         -1.6452        -0.50665
v  ǁVelocityǁ         0.00040278           25.73          7.6861          6.6082
v  Pressure                -523.08          208.27          31.983          36.461
v  k                   9.8593e-011          7.8962         0.22171         0.47407
v  omega                    57.482     2.7319e+008     1.2912e+006           76882
v  TempK                    298.55          363.17          337.16          345.45
v  TurbVisc            2.4707e-018       0.0020838     5.5276e-005      0.00019455
v  CourantNb            0.00020485          1.5549         0.79121         0.97285
v  FourierNb             0.0038133               1         0.41438          0.1711
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.003601      7.397e-005      0.00020233

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.43          306.53
v  Yplus               0          2.9226         0.63028         0.48626


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57397          2.1493          1.2056          1.1439


 INSTANT    0.753000000E-02   TIME STEP NUMBER             753
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924059E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13851E-01 0.46678E+01
   Friction velocity        uk    :  0.13851E-01 0.46639E+01
   Dimensionless distance   yplus :  0.93914E-02 0.29227E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.18243E+03
   Rough dim-less th. sca.  tplus :  0.66529E-02 0.20705E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27437E+00      10   0.12564E-04   0.43513E+01 0.33036E+02 
c  Velocity[X]                                      0.17681E+01 
c  Velocity[Y]                                      0.12054E+01 
c  Velocity[Z]                                      0.13778E+01 
c  Pressure     0.16373E-04      17   0.29332E-03   0.16500E-01 0.11970E+02 
c  k            0.18625E-01      12   0.65969E-04   0.12410E+00 0.53260E+02 
c  omega        0.27922E+07       1   0.91670E-07   0.11297E+08 0.60161E+00 
c  TempK        0.10090E+05       5   0.32894E-05   0.68782E+01 0.92013E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4294e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.08           19.08       0.0064824      -0.0044673
v  Velocity[Y]             -15.555          15.346         0.24058         0.34288
v  Velocity[Z]             -25.568          11.903         -1.6451        -0.50664
v  ǁVelocityǁ         0.00040538          25.732          7.6857          6.6072
v  Pressure                -523.59          208.31          32.022          36.509
v  k                    9.859e-011          7.8922         0.22195          0.4747
v  omega                    57.482     2.7319e+008     1.2912e+006           76881
v  TempK                    298.55          363.17          337.17          345.46
v  TurbVisc            2.4706e-018       0.0020906     5.5353e-005      0.00019481
v  CourantNb            0.00020017          1.5554         0.79119         0.97281
v  FourierNb             0.0038133               1         0.41444         0.17129
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036088     7.3972e-005      0.00020236

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.43          306.53
v  Yplus               0          2.9227         0.63025         0.48622


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.37477          2.1498          1.2056          1.1441


 INSTANT    0.754000000E-02   TIME STEP NUMBER             754
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924073E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13872E-01 0.46677E+01
   Friction velocity        uk    :  0.13872E-01 0.46638E+01
   Dimensionless distance   yplus :  0.94052E-02 0.29228E+01
   Friction thermal sca.    tstar :  0.12142E+01 0.18216E+03
   Rough dim-less th. sca.  tplus :  0.66627E-02 0.20705E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27434E+00      10   0.12486E-04   0.43493E+01 0.33051E+02 
c  Velocity[X]                                      0.17675E+01 
c  Velocity[Y]                                      0.12034E+01 
c  Velocity[Z]                                      0.13784E+01 
c  Pressure     0.16024E-04      17   0.28951E-03   0.16152E-01 0.11854E+02 
c  k            0.18649E-01      12   0.66850E-04   0.12388E+00 0.53247E+02 
c  omega        0.27922E+07       1   0.90557E-07   0.72600E+07 0.52286E+00 
c  TempK        0.10090E+05       5   0.32785E-05   0.68539E+01 0.91933E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.427e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.079          19.081       0.0064414      -0.0044783
v  Velocity[Y]             -15.533          15.349         0.24111          0.3436
v  Velocity[Z]             -25.571          11.897          -1.645        -0.50663
v  ǁVelocityǁ         0.00039839          25.734          7.6853          6.6062
v  Pressure                -524.12          208.34          32.061          36.555
v  k                   9.8586e-011          7.8827         0.22218         0.47533
v  omega                    57.482     2.7319e+008     1.2912e+006           76881
v  TempK                    298.55          363.17          337.18          345.48
v  TurbVisc            2.4705e-018       0.0020964     5.5428e-005      0.00019507
v  CourantNb            0.00020798          1.5559         0.79116         0.97277
v  FourierNb             0.0038134               1         0.41451         0.17149
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036161     7.3974e-005      0.00020238

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.43          306.53
v  Yplus               0          2.9228         0.63022         0.48619


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62936          2.1504          1.2057          1.1443


 INSTANT    0.755000000E-02   TIME STEP NUMBER             755
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924058E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13890E-01 0.46676E+01
   Friction velocity        uk    :  0.13890E-01 0.46637E+01
   Dimensionless distance   yplus :  0.94176E-02 0.29229E+01
   Friction thermal sca.    tstar :  0.12142E+01 0.18192E+03
   Rough dim-less th. sca.  tplus :  0.66715E-02 0.20706E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27431E+00      10   0.12559E-04   0.43382E+01 0.33060E+02 
c  Velocity[X]                                      0.17672E+01 
c  Velocity[Y]                                      0.12024E+01 
c  Velocity[Z]                                      0.13686E+01 
c  Pressure     0.15654E-04      17   0.29274E-03   0.15782E-01 0.11921E+02 
c  k            0.18671E-01      12   0.68024E-04   0.12381E+00 0.53275E+02 
c  omega        0.27922E+07       1   0.91497E-07   0.90930E+07 0.55957E+00 
c  TempK        0.10089E+05       5   0.32678E-05   0.68309E+01 0.91849E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4242e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.077          19.082       0.0063984      -0.0044966
v  Velocity[Y]             -15.561          15.352         0.24165         0.34433
v  Velocity[Z]             -25.573           11.89          -1.645        -0.50661
v  ǁVelocityǁ         0.00039213          25.736           7.685          6.6053
v  Pressure                -524.65          208.38            32.1          36.602
v  k                   9.8582e-011           7.868         0.22242         0.47597
v  omega                    57.482     2.7319e+008     1.2912e+006           76881
v  TempK                    298.56          363.17          337.19          345.49
v  TurbVisc            2.4704e-018       0.0021006     5.5504e-005      0.00019533
v  CourantNb            0.00020828          1.5566         0.79114         0.97273
v  FourierNb             0.0038134               1         0.41458         0.17169
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036228     7.3977e-005       0.0002024

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.43          306.53
v  Yplus               0          2.9229          0.6302         0.48615


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50257          2.1511          1.2057          1.1444


 INSTANT    0.756000000E-02   TIME STEP NUMBER             756
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924072E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13905E-01 0.46676E+01
   Friction velocity        uk    :  0.13905E-01 0.46637E+01
   Dimensionless distance   yplus :  0.94280E-02 0.29229E+01
   Friction thermal sca.    tstar :  0.12142E+01 0.18172E+03
   Rough dim-less th. sca.  tplus :  0.66788E-02 0.20706E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27428E+00      10   0.12519E-04   0.43381E+01 0.33108E+02 
c  Velocity[X]                                      0.17685E+01 
c  Velocity[Y]                                      0.12025E+01 
c  Velocity[Z]                                      0.13671E+01 
c  Pressure     0.15554E-04      18   0.29928E-03   0.15685E-01 0.12175E+02 
c  k            0.18694E-01      12   0.69023E-04   0.12399E+00 0.53341E+02 
c  omega        0.27922E+07       1   0.94207E-07   0.15005E+08 0.66254E+00 
c  TempK        0.10089E+05       5   0.32580E-05   0.68056E+01 0.91771E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4212e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.075          19.083       0.0063533      -0.0045233
v  Velocity[Y]             -15.702          15.355         0.24219         0.34505
v  Velocity[Z]             -25.575          11.883         -1.6449         -0.5066
v  ǁVelocityǁ         0.00038657          25.738          7.6846          6.6043
v  Pressure                -525.18          208.42          32.142          36.651
v  k                   9.8578e-011          7.8546         0.22265          0.4766
v  omega                    57.483     2.7319e+008     1.2912e+006           76881
v  TempK                    298.56          363.17           337.2          345.51
v  TurbVisc            2.4703e-018       0.0021044     5.5579e-005      0.00019559
v  CourantNb            0.00020854          1.5573         0.79111         0.97269
v  FourierNb             0.0038135               1         0.41465         0.17188
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.003629      7.398e-005      0.00020242

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.44          306.53
v  Yplus               0          2.9229         0.63017         0.48612


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.3791          2.1518          1.2058          1.1446


 INSTANT    0.757000000E-02   TIME STEP NUMBER             757
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924123E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13910E-01 0.46675E+01
   Friction velocity        uk    :  0.13910E-01 0.46636E+01
   Dimensionless distance   yplus :  0.94312E-02 0.29230E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.18166E+03
   Rough dim-less th. sca.  tplus :  0.66811E-02 0.20707E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27425E+00      10   0.12481E-04   0.43412E+01 0.33175E+02 
c  Velocity[X]                                      0.17705E+01 
c  Velocity[Y]                                      0.12067E+01 
c  Velocity[Z]                                      0.13641E+01 
c  Pressure     0.15536E-04      17   0.29152E-03   0.15669E-01 0.11549E+02 
c  k            0.18716E-01      12   0.69973E-04   0.12433E+00 0.53442E+02 
c  omega        0.27922E+07       1   0.92705E-07   0.12029E+08 0.61181E+00 
c  TempK        0.10089E+05       5   0.32485E-05   0.67774E+01 0.91653E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4189e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.073          19.084       0.0063044      -0.0045576
v  Velocity[Y]             -15.637          15.358         0.24274         0.34577
v  Velocity[Z]             -25.578          11.875         -1.6448        -0.50659
v  ǁVelocityǁ          0.0003814          25.741          7.6842          6.6033
v  Pressure                -525.72          208.46          32.178          36.694
v  k                   9.8575e-011          7.8375         0.22289         0.47724
v  omega                    57.483     2.7319e+008     1.2912e+006           76880
v  TempK                    298.56          363.17          337.21          345.52
v  TurbVisc            2.4702e-018       0.0021076     5.5655e-005      0.00019585
v  CourantNb            0.00020346          1.5579         0.79109         0.97265
v  FourierNb             0.0038135               1         0.41472         0.17208
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036338     7.3983e-005      0.00020244

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.44          306.53
v  Yplus               0           2.923         0.63014         0.48608


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48643          2.1524          1.2058          1.1447


 INSTANT    0.758000000E-02   TIME STEP NUMBER             758
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923927E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13932E-01 0.46675E+01
   Friction velocity        uk    :  0.13932E-01 0.46635E+01
   Dimensionless distance   yplus :  0.94464E-02 0.29231E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.18137E+03
   Rough dim-less th. sca.  tplus :  0.66919E-02 0.20707E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27422E+00      10   0.12364E-04   0.43341E+01 0.33168E+02 
c  Velocity[X]                                      0.17717E+01 
c  Velocity[Y]                                      0.12005E+01 
c  Velocity[Z]                                      0.13619E+01 
c  Pressure     0.15546E-04      18   0.30028E-03   0.15682E-01 0.11943E+02 
c  k            0.18738E-01      12   0.70855E-04   0.12478E+00 0.53559E+02 
c  omega        0.27922E+07       1   0.93900E-07   0.14502E+08 0.65241E+00 
c  TempK        0.10088E+05       5   0.32388E-05   0.67488E+01 0.91545E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4171e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.072          19.086        0.006253      -0.0045968
v  Velocity[Y]             -15.568           15.36         0.24329          0.3465
v  Velocity[Z]              -25.58          11.866         -1.6448        -0.50658
v  ǁVelocityǁ         0.00037566          25.743          7.6839          6.6024
v  Pressure                -526.27           208.5          32.217          36.741
v  k                   9.8571e-011          7.8155         0.22312         0.47787
v  omega                    57.483     2.7319e+008     1.2912e+006           76880
v  TempK                    298.56          363.17          337.21          345.53
v  TurbVisc            2.4701e-018       0.0021103      5.573e-005      0.00019611
v  CourantNb            0.00019482          1.5583         0.79107         0.97261
v  FourierNb             0.0038135               1         0.41479         0.17228
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036346     7.3985e-005      0.00020246

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.44          306.53
v  Yplus               0          2.9231         0.63011         0.48604


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40171          2.1529          1.2059          1.1449


 INSTANT    0.759000000E-02   TIME STEP NUMBER             759
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923975E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13970E-01 0.46674E+01
   Friction velocity        uk    :  0.13970E-01 0.46635E+01
   Dimensionless distance   yplus :  0.94717E-02 0.29231E+01
   Friction thermal sca.    tstar :  0.12142E+01 0.18088E+03
   Rough dim-less th. sca.  tplus :  0.67098E-02 0.20708E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27419E+00      10   0.12319E-04   0.43394E+01 0.33214E+02 
c  Velocity[X]                                      0.17749E+01 
c  Velocity[Y]                                      0.12010E+01 
c  Velocity[Z]                                      0.13635E+01 
c  Pressure     0.15933E-04      18   0.28380E-03   0.16076E-01 0.11357E+02 
c  k            0.18760E-01      12   0.71427E-04   0.12535E+00 0.53697E+02 
c  omega        0.27922E+07       1   0.93948E-07   0.16314E+08 0.68316E+00 
c  TempK        0.10088E+05       5   0.32290E-05   0.67209E+01 0.91441E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.415e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.07          19.087       0.0061997      -0.0046427
v  Velocity[Y]             -15.539          15.363         0.24384         0.34723
v  Velocity[Z]             -25.581          11.858         -1.6447        -0.50657
v  ǁVelocityǁ         0.00037126          25.744          7.6835          6.6014
v  Pressure                -526.82          208.53           32.25          36.781
v  k                   9.8567e-011          7.7931         0.22335         0.47851
v  omega                    57.483     2.7319e+008     1.2912e+006           76880
v  TempK                    298.56          363.17          337.22          345.55
v  TurbVisc              2.47e-018       0.0021123     5.5805e-005      0.00019637
v  CourantNb            0.00018618          1.5589         0.79104         0.97257
v  FourierNb             0.0038135               1         0.41486         0.17248
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036327     7.3988e-005      0.00020248

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.44          306.53
v  Yplus               0          2.9231         0.63009           0.486


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40078          2.1534          1.2059           1.145


 INSTANT    0.760000000E-02   TIME STEP NUMBER             760
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923891E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13994E-01 0.46674E+01
   Friction velocity        uk    :  0.13994E-01 0.46634E+01
   Dimensionless distance   yplus :  0.94881E-02 0.29232E+01
   Friction thermal sca.    tstar :  0.12142E+01 0.18057E+03
   Rough dim-less th. sca.  tplus :  0.67215E-02 0.20708E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27416E+00      10   0.12303E-04   0.43447E+01 0.33241E+02 
c  Velocity[X]                                      0.17799E+01 
c  Velocity[Y]                                      0.11994E+01 
c  Velocity[Z]                                      0.13654E+01 
c  Pressure     0.15740E-04      17   0.28675E-03   0.15884E-01 0.11099E+02 
c  k            0.18781E-01      12   0.72039E-04   0.12607E+00 0.53861E+02 
c  omega        0.27922E+07       1   0.91525E-07   0.90021E+07 0.55086E+00 
c  TempK        0.10087E+05       5   0.32195E-05   0.66937E+01 0.91319E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4126e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.068          19.088       0.0061435      -0.0046956
v  Velocity[Y]             -15.554          15.366          0.2444         0.34797
v  Velocity[Z]             -25.583          11.851         -1.6446        -0.50656
v  ǁVelocityǁ         0.00036655          25.746          7.6832          6.6005
v  Pressure                -527.36          208.56          32.282           36.82
v  k                   9.8563e-011          7.7789         0.22358         0.47915
v  omega                    57.483     2.7319e+008     1.2912e+006           76879
v  TempK                    298.56          363.17          337.23          345.56
v  TurbVisc            2.4699e-018       0.0021137      5.588e-005      0.00019663
v  CourantNb            0.00017753          1.5594         0.79102         0.97253
v  FourierNb             0.0038135               1         0.41492         0.17268
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.003629     7.3991e-005      0.00020251

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.44          306.53
v  Yplus               0          2.9232         0.63006         0.48596


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39047           2.154          1.2059          1.1452


 INSTANT    0.761000000E-02   TIME STEP NUMBER             761
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923914E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14018E-01 0.46673E+01
   Friction velocity        uk    :  0.14018E-01 0.46634E+01
   Dimensionless distance   yplus :  0.95047E-02 0.29232E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.18026E+03
   Rough dim-less th. sca.  tplus :  0.67332E-02 0.20708E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27413E+00      10   0.12201E-04   0.43313E+01 0.33255E+02 
c  Velocity[X]                                      0.17832E+01 
c  Velocity[Y]                                      0.11969E+01 
c  Velocity[Z]                                      0.13511E+01 
c  Pressure     0.15522E-04      17   0.27898E-03   0.15667E-01 0.10559E+02 
c  k            0.18802E-01      12   0.72970E-04   0.12694E+00 0.54043E+02 
c  omega        0.27922E+07       1   0.92264E-07   0.10626E+08 0.57838E+00 
c  TempK        0.10087E+05       5   0.32102E-05   0.66679E+01 0.91204E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4098e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.067          19.089       0.0060846      -0.0047534
v  Velocity[Y]             -15.619          15.369         0.24496          0.3487
v  Velocity[Z]             -25.585          11.852         -1.6446        -0.50655
v  ǁVelocityǁ         0.00036311          25.748          7.6828          6.5995
v  Pressure                -527.91          208.58          32.307          36.853
v  k                    9.856e-011          7.7602         0.22381         0.47978
v  omega                    57.483     2.7319e+008     1.2912e+006           76879
v  TempK                    298.56          363.17          337.24          345.58
v  TurbVisc            2.4699e-018       0.0021143     5.5954e-005       0.0001969
v  CourantNb            0.00016883          1.5601           0.791         0.97248
v  FourierNb             0.0038135               1         0.41499         0.17288
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036242     7.3994e-005      0.00020253

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.44          306.53
v  Yplus               0          2.9232         0.63003         0.48593


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47644          2.1547           1.206          1.1454


 INSTANT    0.762000000E-02   TIME STEP NUMBER             762
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923695E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14039E-01 0.46673E+01
   Friction velocity        uk    :  0.14039E-01 0.46633E+01
   Dimensionless distance   yplus :  0.95190E-02 0.29233E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.17999E+03
   Rough dim-less th. sca.  tplus :  0.67433E-02 0.20709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27410E+00      10   0.12173E-04   0.43361E+01 0.33324E+02 
c  Velocity[X]                                      0.17876E+01 
c  Velocity[Y]                                      0.11976E+01 
c  Velocity[Z]                                      0.13509E+01 
c  Pressure     0.15692E-04      17   0.28282E-03   0.15842E-01 0.11066E+02 
c  k            0.18823E-01      12   0.73844E-04   0.12781E+00 0.54227E+02 
c  omega        0.27922E+07       1   0.93809E-07   0.13818E+08 0.63285E+00 
c  TempK        0.10086E+05       5   0.32013E-05   0.66442E+01 0.91095E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4069e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.065          19.091       0.0060238      -0.0048182
v  Velocity[Y]             -15.695          15.371         0.24552         0.34943
v  Velocity[Z]             -25.587          11.858         -1.6445        -0.50654
v  ǁVelocityǁ         0.00035934          25.749          7.6825          6.5986
v  Pressure                -528.44          208.61          32.338          36.891
v  k                   9.8556e-011          7.7367         0.22404         0.48042
v  omega                    57.484     2.7319e+008     1.2912e+006           76879
v  TempK                    298.56          363.17          337.25          345.59
v  TurbVisc            2.4698e-018       0.0021142     5.6028e-005      0.00019716
v  CourantNb            0.00015985          1.5608         0.79097         0.97244
v  FourierNb             0.0038135               1         0.41506         0.17308
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036183     7.3997e-005      0.00020255

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.44          306.53
v  Yplus               0          2.9233            0.63         0.48589


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40961          2.1554           1.206          1.1455


 INSTANT    0.763000000E-02   TIME STEP NUMBER             763
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923666E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14051E-01 0.46672E+01
   Friction velocity        uk    :  0.14051E-01 0.46633E+01
   Dimensionless distance   yplus :  0.95268E-02 0.29233E+01
   Friction thermal sca.    tstar :  0.12146E+01 0.17984E+03
   Rough dim-less th. sca.  tplus :  0.67488E-02 0.20709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27407E+00      10   0.12159E-04   0.43402E+01 0.33405E+02 
c  Velocity[X]                                      0.17927E+01 
c  Velocity[Y]                                      0.12018E+01 
c  Velocity[Z]                                      0.13457E+01 
c  Pressure     0.15889E-04      18   0.28648E-03   0.16045E-01 0.10475E+02 
c  k            0.18843E-01      12   0.74661E-04   0.12870E+00 0.54424E+02 
c  omega        0.27922E+07       1   0.93959E-07   0.16588E+08 0.67983E+00 
c  TempK        0.10086E+05       5   0.31924E-05   0.66183E+01 0.90966E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4049e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.064          19.092       0.0059594      -0.0048904
v  Velocity[Y]              -15.66          15.374         0.24608         0.35017
v  Velocity[Z]             -25.588          11.863         -1.6444        -0.50653
v  ǁVelocityǁ         0.00035598          25.751          7.6822          6.5976
v  Pressure                -528.99          208.62           32.36          36.921
v  k                   9.8552e-011           7.708         0.22427         0.48106
v  omega                    57.484     2.7319e+008     1.2912e+006           76879
v  TempK                    298.56          363.17          337.25          345.61
v  TurbVisc            2.4697e-018       0.0021133     5.6103e-005      0.00019742
v  CourantNb            0.00015097          1.5613         0.79094          0.9724
v  FourierNb             0.0038136               1         0.41513         0.17328
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036117        7.4e-005      0.00020257

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.44          306.53
v  Yplus               0          2.9233         0.62998         0.48586


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44041          2.1559          1.2061          1.1457


 INSTANT    0.764000000E-02   TIME STEP NUMBER             764
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923816E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14084E-01 0.46672E+01
   Friction velocity        uk    :  0.14084E-01 0.46633E+01
   Dimensionless distance   yplus :  0.95493E-02 0.29234E+01
   Friction thermal sca.    tstar :  0.12146E+01 0.17941E+03
   Rough dim-less th. sca.  tplus :  0.67648E-02 0.20709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27404E+00      10   0.12158E-04   0.43406E+01 0.33400E+02 
c  Velocity[X]                                      0.17983E+01 
c  Velocity[Y]                                      0.11964E+01 
c  Velocity[Z]                                      0.13459E+01 
c  Pressure     0.16555E-04      16   0.29276E-03   0.16721E-01 0.10331E+02 
c  k            0.18863E-01      12   0.75574E-04   0.12977E+00 0.54636E+02 
c  omega        0.27922E+07       1   0.91823E-07   0.10427E+08 0.56760E+00 
c  TempK        0.10086E+05       5   0.31839E-05   0.65935E+01 0.90843E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4032e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.062          19.093       0.0058935      -0.0049667
v  Velocity[Y]             -15.553          15.376         0.24664         0.35091
v  Velocity[Z]              -25.59          11.867         -1.6444        -0.50653
v  ǁVelocityǁ         0.00035231          25.753          7.6818          6.5967
v  Pressure                -529.56          208.64          32.379          36.948
v  k                   9.8548e-011          7.6738          0.2245          0.4817
v  omega                    57.484     2.7319e+008     1.2912e+006           76878
v  TempK                    298.56          363.17          337.26          345.62
v  TurbVisc            2.4696e-018       0.0021116     5.6177e-005      0.00019769
v  CourantNb            0.00014216          1.5617         0.79092         0.97236
v  FourierNb             0.0038137               1          0.4152         0.17348
v  total_pressure       1.008e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036047     7.4003e-005       0.0002026

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.44          306.53
v  Yplus               0          2.9234         0.62995         0.48582


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.31151          2.1563          1.2061          1.1458


 INSTANT    0.765000000E-02   TIME STEP NUMBER             765
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923811E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14128E-01 0.46672E+01
   Friction velocity        uk    :  0.14128E-01 0.46632E+01
   Dimensionless distance   yplus :  0.95792E-02 0.29234E+01
   Friction thermal sca.    tstar :  0.12142E+01 0.17885E+03
   Rough dim-less th. sca.  tplus :  0.67860E-02 0.20710E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27401E+00      10   0.12143E-04   0.43469E+01 0.33439E+02 
c  Velocity[X]                                      0.18047E+01 
c  Velocity[Y]                                      0.11953E+01 
c  Velocity[Z]                                      0.13469E+01 
c  Pressure     0.16305E-04      16   0.28759E-03   0.16472E-01 0.10039E+02 
c  k            0.18883E-01      12   0.76448E-04   0.13100E+00 0.54861E+02 
c  omega        0.27922E+07       1   0.90454E-07   0.73680E+07 0.50201E+00 
c  TempK        0.10085E+05       5   0.31757E-05   0.65727E+01 0.90734E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4011e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.061          19.095       0.0058282       -0.005048
v  Velocity[Y]             -15.517          15.379         0.24721         0.35165
v  Velocity[Z]             -25.592          11.872         -1.6443        -0.50653
v  ǁVelocityǁ         0.00034933          25.754          7.6815          6.5958
v  Pressure                -530.15          208.64          32.394           36.97
v  k                   9.8544e-011           7.634         0.22473         0.48234
v  omega                    57.484     2.7319e+008     1.2912e+006           76878
v  TempK                    298.56          363.17          337.27          345.63
v  TurbVisc            2.4695e-018       0.0021089     5.6251e-005      0.00019795
v  CourantNb            0.00013347          1.5622         0.79089         0.97232
v  FourierNb             0.0038138               1         0.41527         0.17368
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035975     7.4005e-005      0.00020262

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.44          306.54
v  Yplus               0          2.9234         0.62992         0.48579


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66997          2.1568          1.2062           1.146


 INSTANT    0.766000000E-02   TIME STEP NUMBER             766
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923845E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14159E-01 0.46671E+01
   Friction velocity        uk    :  0.14159E-01 0.46632E+01
   Dimensionless distance   yplus :  0.96000E-02 0.29235E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.17847E+03
   Rough dim-less th. sca.  tplus :  0.68007E-02 0.20710E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27398E+00      10   0.12124E-04   0.43406E+01 0.33483E+02 
c  Velocity[X]                                      0.18110E+01 
c  Velocity[Y]                                      0.11955E+01 
c  Velocity[Z]                                      0.13342E+01 
c  Pressure     0.15796E-04      17   0.28781E-03   0.15961E-01 0.10257E+02 
c  k            0.18903E-01      12   0.77059E-04   0.13229E+00 0.55093E+02 
c  omega        0.27922E+07       1   0.90978E-07   0.84564E+07 0.52141E+00 
c  TempK        0.10085E+05       5   0.31674E-05   0.65527E+01 0.90640E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3988e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.059          19.096        0.005763      -0.0051327
v  Velocity[Y]             -15.544          15.381         0.24779         0.35239
v  Velocity[Z]             -25.593          11.876         -1.6443        -0.50653
v  ǁVelocityǁ         0.00034638          25.756          7.6812          6.5948
v  Pressure                -530.72          208.66          32.414          36.998
v  k                    9.854e-011          7.5886         0.22496         0.48297
v  omega                    57.484     2.7319e+008     1.2912e+006           76878
v  TempK                    298.57          363.17          337.28          345.65
v  TurbVisc            2.4694e-018       0.0021054     5.6325e-005      0.00019822
v  CourantNb            0.00012903          1.5628         0.79087         0.97228
v  FourierNb             0.0038139               1         0.41534         0.17388
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035904     7.4007e-005      0.00020264

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.44          306.54
v  Yplus               0          2.9235          0.6299         0.48575


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61298          2.1574          1.2062          1.1462


 INSTANT    0.767000000E-02   TIME STEP NUMBER             767
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923921E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14190E-01 0.46671E+01
   Friction velocity        uk    :  0.14190E-01 0.46632E+01
   Dimensionless distance   yplus :  0.96210E-02 0.29235E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.17808E+03
   Rough dim-less th. sca.  tplus :  0.68156E-02 0.20710E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27395E+00      10   0.12124E-04   0.43531E+01 0.33581E+02 
c  Velocity[X]                                      0.18191E+01 
c  Velocity[Y]                                      0.11999E+01 
c  Velocity[Z]                                      0.13341E+01 
c  Pressure     0.15885E-04      17   0.29137E-03   0.16054E-01 0.10459E+02 
c  k            0.18922E-01      12   0.77554E-04   0.13355E+00 0.55317E+02 
c  omega        0.27922E+07       1   0.95041E-07   0.17883E+08 0.68777E+00 
c  TempK        0.10084E+05       5   0.31596E-05   0.65353E+01 0.90562E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3961e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.058          19.098       0.0056996       -0.005222
v  Velocity[Y]             -15.678          15.383         0.24836         0.35313
v  Velocity[Z]             -25.595           11.88         -1.6442        -0.50653
v  ǁVelocityǁ         0.00034404          25.757          7.6809          6.5939
v  Pressure                 -531.3          208.68          32.436          37.028
v  k                   9.8537e-011          7.5375         0.22518         0.48361
v  omega                    57.484     2.7319e+008     1.2912e+006           76877
v  TempK                    298.57          363.17          337.29          345.66
v  TurbVisc            2.4693e-018       0.0021009     5.6399e-005      0.00019848
v  CourantNb            0.00012957          1.5634         0.79084         0.97224
v  FourierNb              0.003814               1         0.41541         0.17408
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035832      7.401e-005      0.00020266

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.44          306.54
v  Yplus               0          2.9235         0.62988         0.48572


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47404          2.1581          1.2063          1.1463


 INSTANT    0.768000000E-02   TIME STEP NUMBER             768
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923899E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14211E-01 0.46671E+01
   Friction velocity        uk    :  0.14211E-01 0.46631E+01
   Dimensionless distance   yplus :  0.96351E-02 0.29235E+01
   Friction thermal sca.    tstar :  0.12147E+01 0.17782E+03
   Rough dim-less th. sca.  tplus :  0.68256E-02 0.20710E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27392E+00      10   0.12128E-04   0.43615E+01 0.33666E+02 
c  Velocity[X]                                      0.18262E+01 
c  Velocity[Y]                                      0.12060E+01 
c  Velocity[Z]                                      0.13293E+01 
c  Pressure     0.15887E-04      17   0.28947E-03   0.16060E-01 0.99226E+01 
c  k            0.18942E-01      12   0.77997E-04   0.13475E+00 0.55525E+02 
c  omega        0.27922E+07       1   0.92540E-07   0.12290E+08 0.59157E+00 
c  TempK        0.10084E+05       5   0.31517E-05   0.65151E+01 0.90444E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3939e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.056          19.099       0.0056349      -0.0053181
v  Velocity[Y]             -15.678          15.385         0.24894         0.35387
v  Velocity[Z]             -25.596          11.883         -1.6442        -0.50653
v  ǁVelocityǁ         0.00034182          25.758          7.6805           6.593
v  Pressure                -531.89          208.69          32.449          37.048
v  k                   9.8533e-011          7.4806         0.22541         0.48425
v  omega                    57.485     2.7318e+008     1.2912e+006           76877
v  TempK                    298.57          363.17          337.29          345.68
v  TurbVisc            2.4692e-018       0.0020954     5.6471e-005      0.00019875
v  CourantNb             0.0001299           1.564         0.79082          0.9722
v  FourierNb             0.0038141               1         0.41547         0.17428
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035757     7.4013e-005      0.00020268

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.44          306.54
v  Yplus               0          2.9235         0.62985         0.48569


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41171          2.1586          1.2063          1.1465


 INSTANT    0.769000000E-02   TIME STEP NUMBER             769
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923972E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14237E-01 0.46670E+01
   Friction velocity        uk    :  0.14237E-01 0.46631E+01
   Dimensionless distance   yplus :  0.96529E-02 0.29235E+01
   Friction thermal sca.    tstar :  0.12147E+01 0.17749E+03
   Rough dim-less th. sca.  tplus :  0.68381E-02 0.20711E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27389E+00      10   0.12089E-04   0.43581E+01 0.33659E+02 
c  Velocity[X]                                      0.18297E+01 
c  Velocity[Y]                                      0.12012E+01 
c  Velocity[Z]                                      0.13271E+01 
c  Pressure     0.15871E-04      16   0.28404E-03   0.16047E-01 0.97163E+01 
c  k            0.18961E-01      12   0.78415E-04   0.13590E+00 0.55712E+02 
c  omega        0.27922E+07       1   0.91315E-07   0.96176E+07 0.53929E+00 
c  TempK        0.10083E+05       5   0.31439E-05   0.64935E+01 0.90346E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3923e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.055            19.1       0.0055696      -0.0054177
v  Velocity[Y]              -15.63          15.388         0.24952         0.35461
v  Velocity[Z]             -25.597          11.886         -1.6441        -0.50653
v  ǁVelocityǁ         0.00033996          25.759          7.6802          6.5921
v  Pressure                -532.49          208.68          32.453           37.06
v  k                   9.8529e-011          7.4181         0.22563         0.48488
v  omega                    57.485     2.7318e+008     1.2912e+006           76877
v  TempK                    298.57          363.17           337.3          345.69
v  TurbVisc            2.4691e-018       0.0020887     5.6544e-005      0.00019901
v  CourantNb             0.0001303          1.5644          0.7908         0.97216
v  FourierNb             0.0038142               1         0.41554         0.17447
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035683     7.4016e-005      0.00020269

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.45          306.54
v  Yplus               0          2.9235         0.62983         0.48565


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4209           2.159          1.2063          1.1466


 INSTANT    0.770000000E-02   TIME STEP NUMBER             770
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923869E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14288E-01 0.46670E+01
   Friction velocity        uk    :  0.14288E-01 0.46631E+01
   Dimensionless distance   yplus :  0.96875E-02 0.29236E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.17685E+03
   Rough dim-less th. sca.  tplus :  0.68627E-02 0.20711E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27386E+00      10   0.12082E-04   0.43590E+01 0.33685E+02 
c  Velocity[X]                                      0.18339E+01 
c  Velocity[Y]                                      0.11995E+01 
c  Velocity[Z]                                      0.13256E+01 
c  Pressure     0.15560E-04      16   0.28186E-03   0.15737E-01 0.97572E+01 
c  k            0.18980E-01      12   0.78554E-04   0.13698E+00 0.55878E+02 
c  omega        0.27922E+07       1   0.91066E-07   0.93248E+07 0.53268E+00 
c  TempK        0.10083E+05       5   0.31360E-05   0.64739E+01 0.90259E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3906e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.054          19.102       0.0055042      -0.0055255
v  Velocity[Y]             -15.557           15.39          0.2501         0.35536
v  Velocity[Z]             -25.598          11.888         -1.6441        -0.50653
v  ǁVelocityǁ         0.00033793           25.76          7.6799          6.5911
v  Pressure                -533.09          208.68           32.46          37.075
v  k                   9.8525e-011          7.3502         0.22586         0.48552
v  omega                    57.485     2.7318e+008     1.2912e+006           76876
v  TempK                    298.57          363.17          337.31           345.7
v  TurbVisc             2.469e-018       0.0020824     5.6617e-005      0.00019928
v  CourantNb             0.0001306          1.5648         0.79077         0.97211
v  FourierNb             0.0038143               1         0.41561         0.17467
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035606     7.4018e-005      0.00020271

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.45          306.54
v  Yplus               0          2.9236          0.6298         0.48562


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52513          2.1595          1.2064          1.1468


 INSTANT    0.771000000E-02   TIME STEP NUMBER             771
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923875E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14334E-01 0.46670E+01
   Friction velocity        uk    :  0.14334E-01 0.46630E+01
   Dimensionless distance   yplus :  0.97189E-02 0.29236E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.17628E+03
   Rough dim-less th. sca.  tplus :  0.68849E-02 0.20711E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27383E+00      10   0.12096E-04   0.43626E+01 0.33733E+02 
c  Velocity[X]                                      0.18396E+01 
c  Velocity[Y]                                      0.12003E+01 
c  Velocity[Z]                                      0.13228E+01 
c  Pressure     0.15543E-04      16   0.28173E-03   0.15722E-01 0.97951E+01 
c  k            0.18999E-01      12   0.78662E-04   0.13795E+00 0.56020E+02 
c  omega        0.27922E+07       1   0.89999E-07   0.67600E+07 0.47528E+00 
c  TempK        0.10083E+05       5   0.31279E-05   0.64566E+01 0.90172E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3886e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.052          19.103       0.0054373      -0.0056353
v  Velocity[Y]             -15.538          15.392         0.25068          0.3561
v  Velocity[Z]             -25.599           11.89          -1.644        -0.50653
v  ǁVelocityǁ          0.0003364          25.761          7.6796          6.5902
v  Pressure                -533.68          208.69          32.469          37.092
v  k                   9.8521e-011          7.2886         0.22608         0.48615
v  omega                    57.485     2.7318e+008     1.2912e+006           76876
v  TempK                    298.57          363.17          337.32          345.72
v  TurbVisc            2.4689e-018       0.0020801      5.669e-005      0.00019954
v  CourantNb            0.00013073          1.5653         0.79074         0.97207
v  FourierNb             0.0038144               1         0.41568         0.17486
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035524     7.4021e-005      0.00020273

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.45          306.54
v  Yplus               0          2.9236         0.62978         0.48559


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39745            2.16          1.2064          1.1469


 INSTANT    0.772000000E-02   TIME STEP NUMBER             772
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923963E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14376E-01 0.46669E+01
   Friction velocity        uk    :  0.14376E-01 0.46630E+01
   Dimensionless distance   yplus :  0.97473E-02 0.29236E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.17577E+03
   Rough dim-less th. sca.  tplus :  0.69051E-02 0.20711E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27380E+00      10   0.12105E-04   0.43670E+01 0.33782E+02 
c  Velocity[X]                                      0.18441E+01 
c  Velocity[Y]                                      0.12001E+01 
c  Velocity[Z]                                      0.13227E+01 
c  Pressure     0.15375E-04      16   0.27659E-03   0.15556E-01 0.96975E+01 
c  k            0.19017E-01      12   0.78812E-04   0.13887E+00 0.56149E+02 
c  omega        0.27922E+07       1   0.89827E-07   0.66260E+07 0.47129E+00 
c  TempK        0.10082E+05       5   0.31198E-05   0.64375E+01 0.90080E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3862e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.051          19.104       0.0053718      -0.0057491
v  Velocity[Y]              -15.56          15.394         0.25127         0.35685
v  Velocity[Z]             -25.601          11.892         -1.6439        -0.50654
v  ǁVelocityǁ         0.00033474          25.763          7.6793          6.5893
v  Pressure                -534.27          208.69          32.476          37.106
v  k                   9.8517e-011          7.2342          0.2263         0.48678
v  omega                    57.485     2.7318e+008     1.2912e+006           76876
v  TempK                    298.57          363.17          337.32          345.73
v  TurbVisc            2.4688e-018       0.0020763     5.6763e-005      0.00019981
v  CourantNb            0.00013083          1.5659         0.79072         0.97202
v  FourierNb             0.0038145               1         0.41574         0.17506
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035436     7.4024e-005      0.00020275

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.45          306.54
v  Yplus               0          2.9236         0.62976         0.48555


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42231          2.1606          1.2065          1.1471


 INSTANT    0.773000000E-02   TIME STEP NUMBER             773
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924079E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14418E-01 0.46669E+01
   Friction velocity        uk    :  0.14418E-01 0.46630E+01
   Dimensionless distance   yplus :  0.97753E-02 0.29237E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.17527E+03
   Rough dim-less th. sca.  tplus :  0.69249E-02 0.20712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27377E+00      10   0.12132E-04   0.43763E+01 0.33868E+02 
c  Velocity[X]                                      0.18498E+01 
c  Velocity[Y]                                      0.12012E+01 
c  Velocity[Z]                                      0.13253E+01 
c  Pressure     0.15352E-04      16   0.27095E-03   0.15536E-01 0.10030E+02 
c  k            0.19036E-01      12   0.79004E-04   0.13970E+00 0.56258E+02 
c  omega        0.27922E+07       1   0.94799E-07   0.16738E+08 0.66265E+00 
c  TempK        0.10082E+05       5   0.31118E-05   0.64202E+01 0.90017E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3835e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.05          19.105       0.0053038      -0.0058645
v  Velocity[Y]             -15.718          15.396         0.25185         0.35759
v  Velocity[Z]             -25.602          11.893         -1.6439        -0.50655
v  ǁVelocityǁ         0.00033382          25.764           7.679          6.5884
v  Pressure                -534.85          208.69          32.484          37.121
v  k                   9.8513e-011          7.5918         0.22653         0.48741
v  omega                    57.486     2.7318e+008     1.2912e+006           76876
v  TempK                    298.57          363.17          337.33          345.75
v  TurbVisc            2.4687e-018        0.002061     5.6835e-005      0.00020008
v  CourantNb            0.00013095          1.5665          0.7907         0.97198
v  FourierNb             0.0038146               1         0.41581         0.17525
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035352     7.4026e-005      0.00020276

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.45          306.54
v  Yplus               0          2.9237         0.62974         0.48553


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.37395          2.1612          1.2065          1.1472


 INSTANT    0.774000000E-02   TIME STEP NUMBER             774
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923993E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14437E-01 0.46669E+01
   Friction velocity        uk    :  0.14437E-01 0.46630E+01
   Dimensionless distance   yplus :  0.97887E-02 0.29237E+01
   Friction thermal sca.    tstar :  0.12148E+01 0.17503E+03
   Rough dim-less th. sca.  tplus :  0.69343E-02 0.20712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27373E+00      10   0.12183E-04   0.43915E+01 0.33993E+02 
c  Velocity[X]                                      0.18569E+01 
c  Velocity[Y]                                      0.12119E+01 
c  Velocity[Z]                                      0.13228E+01 
c  Pressure     0.15365E-04      16   0.27358E-03   0.15552E-01 0.98658E+01 
c  k            0.19055E-01      12   0.78839E-04   0.14044E+00 0.56347E+02 
c  omega        0.27922E+07       1   0.93477E-07   0.16106E+08 0.65522E+00 
c  TempK        0.10081E+05       5   0.31041E-05   0.63986E+01 0.89904E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3816e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.048          19.107       0.0052378      -0.0059867
v  Velocity[Y]             -15.671          15.398         0.25243         0.35834
v  Velocity[Z]             -25.602          11.894         -1.6439        -0.50656
v  ǁVelocityǁ         0.00033313          25.764          7.6787          6.5875
v  Pressure                -535.44          208.69           32.49          37.134
v  k                   9.8509e-011          7.9818         0.22675         0.48804
v  omega                    57.486     2.7318e+008     1.2912e+006           76875
v  TempK                    298.57          363.17          337.34          345.76
v  TurbVisc            2.4686e-018       0.0020536     5.6908e-005      0.00020034
v  CourantNb            0.00013099           1.567         0.79067         0.97193
v  FourierNb             0.0038147               1         0.41588         0.17545
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035267     7.4028e-005      0.00020278

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.45          306.54
v  Yplus               0          2.9237         0.62973          0.4855


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6471          2.1617          1.2065          1.1474


 INSTANT    0.775000000E-02   TIME STEP NUMBER             775
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923969E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14484E-01 0.46669E+01
   Friction velocity        uk    :  0.14484E-01 0.46630E+01
   Dimensionless distance   yplus :  0.98202E-02 0.29237E+01
   Friction thermal sca.    tstar :  0.12147E+01 0.17446E+03
   Rough dim-less th. sca.  tplus :  0.69567E-02 0.20711E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27370E+00      10   0.12212E-04   0.43892E+01 0.33981E+02 
c  Velocity[X]                                      0.18626E+01 
c  Velocity[Y]                                      0.12077E+01 
c  Velocity[Z]                                      0.13189E+01 
c  Pressure     0.15505E-04      16   0.27137E-03   0.15696E-01 0.98277E+01 
c  k            0.19073E-01      12   0.78269E-04   0.14105E+00 0.56406E+02 
c  omega        0.27922E+07       1   0.92590E-07   0.13541E+08 0.61173E+00 
c  TempK        0.10081E+05       5   0.30964E-05   0.63785E+01 0.89803E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3802e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.047          19.108       0.0051669      -0.0061144
v  Velocity[Y]             -15.593            15.4         0.25302         0.35908
v  Velocity[Z]             -25.603          11.894         -1.6438        -0.50657
v  ǁVelocityǁ         0.00033261          25.765          7.6785          6.5867
v  Pressure                -536.04          208.68           32.49          37.142
v  k                   9.8505e-011          8.2323         0.22697         0.48866
v  omega                    57.486     2.7318e+008     1.2912e+006           76875
v  TempK                    298.57          363.17          337.35          345.77
v  TurbVisc            2.4685e-018       0.0020561     5.6981e-005      0.00020061
v  CourantNb            0.00013084          1.5674         0.79065         0.97189
v  FourierNb             0.0038148               1         0.41594         0.17564
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035166      7.403e-005       0.0002028

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.45          306.54
v  Yplus               0          2.9237         0.62971         0.48547


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44029           2.162          1.2066          1.1475


 INSTANT    0.776000000E-02   TIME STEP NUMBER             776
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924298E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14550E-01 0.46669E+01
   Friction velocity        uk    :  0.14550E-01 0.46629E+01
   Dimensionless distance   yplus :  0.98653E-02 0.29237E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.17367E+03
   Rough dim-less th. sca.  tplus :  0.69887E-02 0.20712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27367E+00      10   0.12237E-04   0.43920E+01 0.33995E+02 
c  Velocity[X]                                      0.18681E+01 
c  Velocity[Y]                                      0.12065E+01 
c  Velocity[Z]                                      0.13173E+01 
c  Pressure     0.15539E-04      16   0.26994E-03   0.15732E-01 0.97872E+01 
c  k            0.19091E-01      12   0.77757E-04   0.14152E+00 0.56432E+02 
c  omega        0.27922E+07       1   0.90232E-07   0.72248E+07 0.48712E+00 
c  TempK        0.10080E+05       5   0.30891E-05   0.63583E+01 0.89710E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3786e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.046           19.11       0.0050964      -0.0062448
v  Velocity[Y]             -15.559          15.402          0.2536         0.35982
v  Velocity[Z]             -25.604          11.894         -1.6438        -0.50659
v  ǁVelocityǁ         0.00033145          25.766          7.6782          6.5858
v  Pressure                -536.66          208.67          32.487          37.146
v  k                   9.8501e-011          8.3594         0.22719         0.48929
v  omega                    57.486     2.7318e+008     1.2912e+006           76875
v  TempK                    298.57          363.17          337.36          345.79
v  TurbVisc            2.4684e-018       0.0020579     5.7054e-005      0.00020088
v  CourantNb             0.0001306          1.5677         0.79062         0.97184
v  FourierNb             0.0038149               1         0.41601         0.17583
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035059     7.4032e-005      0.00020281

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.45          306.54
v  Yplus               0          2.9237         0.62969         0.48545


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57934          2.1624          1.2066          1.1477


 INSTANT    0.777000000E-02   TIME STEP NUMBER             777
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924743E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14603E-01 0.46668E+01
   Friction velocity        uk    :  0.14603E-01 0.46629E+01
   Dimensionless distance   yplus :  0.99012E-02 0.29237E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.17304E+03
   Rough dim-less th. sca.  tplus :  0.70141E-02 0.20712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27364E+00      10   0.12251E-04   0.44073E+01 0.34053E+02 
c  Velocity[X]                                      0.18741E+01 
c  Velocity[Y]                                      0.12086E+01 
c  Velocity[Z]                                      0.13246E+01 
c  Pressure     0.16226E-04      16   0.26737E-03   0.16429E-01 0.99447E+01 
c  k            0.19109E-01      12   0.77618E-04   0.14183E+00 0.56433E+02 
c  omega        0.27922E+07       1   0.90309E-07   0.70266E+07 0.48595E+00 
c  TempK        0.10080E+05       5   0.30814E-05   0.63408E+01 0.89626E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3767e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.045          19.112        0.005024      -0.0063784
v  Velocity[Y]             -15.567          15.404         0.25419         0.36056
v  Velocity[Z]             -25.605          11.894         -1.6437         -0.5066
v  ǁVelocityǁ         0.00033126          25.766          7.6779          6.5849
v  Pressure                -537.28          208.66           32.48          37.147
v  k                   9.8497e-011          8.3858         0.22741          0.4899
v  omega                    57.486     2.7318e+008     1.2912e+006           76874
v  TempK                    298.57          363.17          337.36           345.8
v  TurbVisc            2.4683e-018       0.0020603     5.7126e-005      0.00020114
v  CourantNb             0.0001306          1.5682          0.7906          0.9718
v  FourierNb             0.0038149               1         0.41607         0.17602
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034953     7.4034e-005      0.00020283

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.45          306.54
v  Yplus               0          2.9237         0.62967         0.48542


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.25432          2.1629          1.2067          1.1478


 INSTANT    0.778000000E-02   TIME STEP NUMBER             778
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925119E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14651E-01 0.46668E+01
   Friction velocity        uk    :  0.14651E-01 0.46629E+01
   Dimensionless distance   yplus :  0.99336E-02 0.29237E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.17247E+03
   Rough dim-less th. sca.  tplus :  0.70370E-02 0.20712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27360E+00      10   0.12256E-04   0.44259E+01 0.34131E+02 
c  Velocity[X]                                      0.18804E+01 
c  Velocity[Y]                                      0.12105E+01 
c  Velocity[Z]                                      0.13350E+01 
c  Pressure     0.15796E-04      16   0.27223E-03   0.15997E-01 0.10017E+02 
c  k            0.19127E-01      12   0.77291E-04   0.14202E+00 0.56411E+02 
c  omega        0.27922E+07       1   0.92490E-07   0.11111E+08 0.57105E+00 
c  TempK        0.10079E+05       5   0.30746E-05   0.63235E+01 0.89545E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3745e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.044          19.113       0.0049545      -0.0065183
v  Velocity[Y]             -15.654          15.406         0.25477          0.3613
v  Velocity[Z]             -25.605          11.894         -1.6437        -0.50661
v  ǁVelocityǁ         0.00033105          25.767          7.6776           6.584
v  Pressure                 -537.9          208.64           32.47          37.144
v  k                   9.8493e-011          8.3457         0.22763         0.49052
v  omega                    57.487     2.7318e+008     1.2912e+006           76874
v  TempK                    298.58          363.17          337.37          345.81
v  TurbVisc            2.4682e-018       0.0020629     5.7198e-005       0.0002014
v  CourantNb            0.00013037          1.5687         0.79057         0.97175
v  FourierNb              0.003815               1         0.41614         0.17621
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034842     7.4034e-005      0.00020284

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.45          306.54
v  Yplus               0          2.9237         0.62966          0.4854


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5662          2.1635          1.2067           1.148


 INSTANT    0.779000000E-02   TIME STEP NUMBER             779
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925285E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14687E-01 0.46668E+01
   Friction velocity        uk    :  0.14687E-01 0.46629E+01
   Dimensionless distance   yplus :  0.99581E-02 0.29237E+01
   Friction thermal sca.    tstar :  0.12146E+01 0.17205E+03
   Rough dim-less th. sca.  tplus :  0.70544E-02 0.20712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27357E+00      10   0.12276E-04   0.44264E+01 0.34197E+02 
c  Velocity[X]                                      0.18886E+01 
c  Velocity[Y]                                      0.12151E+01 
c  Velocity[Z]                                      0.13228E+01 
c  Pressure     0.15905E-04      16   0.26990E-03   0.16111E-01 0.99699E+01 
c  k            0.19145E-01      12   0.76594E-04   0.14208E+00 0.56367E+02 
c  omega        0.27922E+07       1   0.95243E-07   0.19639E+08 0.71861E+00 
c  TempK        0.10079E+05       5   0.30668E-05   0.63077E+01 0.89478E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3722e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.042          19.115        0.004883      -0.0066614
v  Velocity[Y]             -15.709          15.407         0.25535         0.36203
v  Velocity[Z]             -25.606          11.893         -1.6436        -0.50663
v  ǁVelocityǁ         0.00033181          25.768          7.6774          6.5832
v  Pressure                -538.51          208.63          32.461          37.142
v  k                   9.8489e-011          8.2673         0.22785         0.49114
v  omega                    57.487     2.7318e+008     1.2912e+006           76874
v  TempK                    298.58          363.17          337.38          345.83
v  TurbVisc            2.4681e-018       0.0020646     5.7269e-005      0.00020167
v  CourantNb            0.00012998          1.5693         0.79055         0.97171
v  FourierNb             0.0038151               1          0.4162         0.17639
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034724     7.4035e-005      0.00020284

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.45          306.54
v  Yplus               0          2.9237         0.62964         0.48538


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65895           2.164          1.2068          1.1481


 INSTANT    0.780000000E-02   TIME STEP NUMBER             780
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925246E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14725E-01 0.46668E+01
   Friction velocity        uk    :  0.14725E-01 0.46629E+01
   Dimensionless distance   yplus :  0.99841E-02 0.29237E+01
   Friction thermal sca.    tstar :  0.12148E+01 0.17160E+03
   Rough dim-less th. sca.  tplus :  0.70728E-02 0.20712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27354E+00      10   0.12270E-04   0.44435E+01 0.34294E+02 
c  Velocity[X]                                      0.18948E+01 
c  Velocity[Y]                                      0.12220E+01 
c  Velocity[Z]                                      0.13268E+01 
c  Pressure     0.15887E-04      16   0.27890E-03   0.16097E-01 0.10070E+02 
c  k            0.19163E-01      12   0.75729E-04   0.14201E+00 0.56306E+02 
c  omega        0.27922E+07       1   0.94676E-07   0.17393E+08 0.68485E+00 
c  TempK        0.10078E+05       5   0.30597E-05   0.62910E+01 0.89397E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3708e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.041          19.117       0.0048075       -0.006809
v  Velocity[Y]             -15.638          15.409         0.25593         0.36277
v  Velocity[Z]             -25.607          11.893         -1.6435        -0.50665
v  ǁVelocityǁ         0.00033192          25.768          7.6771          6.5823
v  Pressure                -539.14          208.61          32.453          37.141
v  k                   9.8484e-011          8.1718         0.22807         0.49175
v  omega                    57.487     2.7318e+008     1.2912e+006           76874
v  TempK                    298.58          363.17          337.39          345.84
v  TurbVisc             2.468e-018       0.0020654     5.7341e-005      0.00020193
v  CourantNb            0.00012947          1.5697         0.79052         0.97167
v  FourierNb             0.0038152               1         0.41627         0.17658
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034617     7.4035e-005      0.00020285

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.45          306.55
v  Yplus               0          2.9237         0.62963         0.48536


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35599          2.1644          1.2068          1.1482


 INSTANT    0.781000000E-02   TIME STEP NUMBER             781
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925252E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14795E-01 0.46668E+01
   Friction velocity        uk    :  0.14795E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10031E-01 0.29237E+01
   Friction thermal sca.    tstar :  0.12147E+01 0.17079E+03
   Rough dim-less th. sca.  tplus :  0.71063E-02 0.20712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27350E+00      10   0.12322E-04   0.44528E+01 0.34332E+02 
c  Velocity[X]                                      0.19040E+01 
c  Velocity[Y]                                      0.12228E+01 
c  Velocity[Z]                                      0.13260E+01 
c  Pressure     0.16161E-04      16   0.26996E-03   0.16377E-01 0.10162E+02 
c  k            0.19181E-01      12   0.75008E-04   0.14183E+00 0.56226E+02 
c  omega        0.27922E+07       1   0.92898E-07   0.12827E+08 0.60796E+00 
c  TempK        0.10078E+05       5   0.30524E-05   0.62725E+01 0.89325E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3695e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.04          19.119       0.0047337      -0.0069577
v  Velocity[Y]             -15.581          15.411         0.25651          0.3635
v  Velocity[Z]             -25.607            11.9         -1.6435        -0.50668
v  ǁVelocityǁ         0.00033251          25.769          7.6769          6.5814
v  Pressure                -539.78           208.6          32.442          37.137
v  k                    9.848e-011          8.0717         0.22828         0.49236
v  omega                    57.487     2.7318e+008     1.2912e+006           76873
v  TempK                    298.58          363.17          337.39          345.85
v  TurbVisc            2.4679e-018       0.0020652     5.7412e-005      0.00020219
v  CourantNb            0.00012889            1.57          0.7905         0.97162
v  FourierNb             0.0038152               1         0.41633         0.17676
v  total_pressure      1.0079e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034498     7.4034e-005      0.00020285

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.45          306.55
v  Yplus               0          2.9237         0.62961         0.48533


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60257          2.1647          1.2068          1.1484


 INSTANT    0.782000000E-02   TIME STEP NUMBER             782
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925435E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14864E-01 0.46668E+01
   Friction velocity        uk    :  0.14864E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10078E-01 0.29237E+01
   Friction thermal sca.    tstar :  0.12142E+01 0.17000E+03
   Rough dim-less th. sca.  tplus :  0.71392E-02 0.20712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27347E+00      10   0.12350E-04   0.44655E+01 0.34376E+02 
c  Velocity[X]                                      0.19108E+01 
c  Velocity[Y]                                      0.12263E+01 
c  Velocity[Z]                                      0.13284E+01 
c  Pressure     0.16327E-04      16   0.27892E-03   0.16548E-01 0.10628E+02 
c  k            0.19199E-01      12   0.74296E-04   0.14162E+00 0.56136E+02 
c  omega        0.27922E+07       1   0.92027E-07   0.93025E+07 0.54457E+00 
c  TempK        0.10078E+05       5   0.30454E-05   0.62558E+01 0.89243E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3678e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.039          19.121       0.0046579      -0.0071101
v  Velocity[Y]             -15.571          15.413         0.25708         0.36424
v  Velocity[Z]             -25.607          11.906         -1.6434         -0.5067
v  ǁVelocityǁ          0.0003335          25.769          7.6766          6.5806
v  Pressure                -540.43          208.57          32.421          37.124
v  k                   9.8476e-011          7.9745          0.2285         0.49297
v  omega                    57.487     2.7318e+008     1.2912e+006           76873
v  TempK                    298.58          363.17           337.4          345.87
v  TurbVisc            2.4678e-018       0.0020643     5.7484e-005      0.00020245
v  CourantNb            0.00012823          1.5704         0.79048         0.97157
v  FourierNb             0.0038152               1         0.41639         0.17694
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034365     7.4033e-005      0.00020286

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.45          306.55
v  Yplus               0          2.9237         0.62959         0.48531


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49047          2.1651          1.2069          1.1485


 INSTANT    0.783000000E-02   TIME STEP NUMBER             783
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925636E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14919E-01 0.46668E+01
   Friction velocity        uk    :  0.14919E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10115E-01 0.29237E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.16938E+03
   Rough dim-less th. sca.  tplus :  0.71656E-02 0.20712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27343E+00      10   0.12379E-04   0.44714E+01 0.34404E+02 
c  Velocity[X]                                      0.19153E+01 
c  Velocity[Y]                                      0.12268E+01 
c  Velocity[Z]                                      0.13293E+01 
c  Pressure     0.16516E-04      16   0.28893E-03   0.16744E-01 0.10974E+02 
c  k            0.19216E-01      12   0.73680E-04   0.14135E+00 0.56034E+02 
c  omega        0.27922E+07       1   0.92618E-07   0.10017E+08 0.56239E+00 
c  TempK        0.10077E+05       5   0.30384E-05   0.62372E+01 0.89169E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3659e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.038          19.123       0.0045801      -0.0072664
v  Velocity[Y]             -15.607          15.415         0.25766         0.36497
v  Velocity[Z]             -25.607          11.913         -1.6434        -0.50672
v  ǁVelocityǁ          0.0003344          25.769          7.6764          6.5797
v  Pressure                -541.08          208.54          32.396          37.105
v  k                   9.8471e-011          7.8834         0.22871         0.49357
v  omega                    57.488     2.7318e+008     1.2912e+006           76873
v  TempK                    298.58          363.17          337.41          345.88
v  TurbVisc            2.4677e-018       0.0020626     5.7555e-005      0.00020271
v  CourantNb            0.00010824          1.5709         0.79045         0.97153
v  FourierNb             0.0038153               1         0.41645         0.17712
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034228     7.4032e-005      0.00020286

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.45          306.55
v  Yplus               0          2.9237         0.62958         0.48529


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5504          2.1656          1.2069          1.1487


 INSTANT    0.784000000E-02   TIME STEP NUMBER             784
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925612E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14971E-01 0.46668E+01
   Friction velocity        uk    :  0.14970E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10150E-01 0.29237E+01
   Friction thermal sca.    tstar :  0.12145E+01 0.16879E+03
   Rough dim-less th. sca.  tplus :  0.71905E-02 0.20712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27340E+00      10   0.12419E-04   0.44804E+01 0.34468E+02 
c  Velocity[X]                                      0.19176E+01 
c  Velocity[Y]                                      0.12299E+01 
c  Velocity[Z]                                      0.13328E+01 
c  Pressure     0.16422E-04      16   0.29309E-03   0.16651E-01 0.10865E+02 
c  k            0.19234E-01      12   0.72515E-04   0.14105E+00 0.55920E+02 
c  omega        0.27922E+07       1   0.95329E-07   0.15344E+08 0.66065E+00 
c  TempK        0.10077E+05       5   0.30314E-05   0.62133E+01 0.89103E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3638e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.037          19.125       0.0045037      -0.0074179
v  Velocity[Y]              -15.76          15.416         0.25822         0.36571
v  Velocity[Z]             -25.607          11.919         -1.6433        -0.50674
v  ǁVelocityǁ          0.0003363          25.769          7.6761          6.5788
v  Pressure                -541.72          208.52          32.383          37.099
v  k                   9.8467e-011             7.8         0.22893         0.49417
v  omega                    57.488     2.7318e+008     1.2912e+006           76872
v  TempK                    298.58          363.17          337.42          345.89
v  TurbVisc            2.4676e-018       0.0020602     5.7626e-005      0.00020297
v  CourantNb            0.00011553          1.5714         0.79043         0.97149
v  FourierNb             0.0038153               1         0.41652         0.17731
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034079      7.403e-005      0.00020287

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.55
v  Yplus               0          2.9237         0.62957         0.48526


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42677          2.1662          1.2069          1.1488


 INSTANT    0.785000000E-02   TIME STEP NUMBER             785
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925687E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15003E-01 0.46668E+01
   Friction velocity        uk    :  0.15003E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10172E-01 0.29237E+01
   Friction thermal sca.    tstar :  0.12150E+01 0.16843E+03
   Rough dim-less th. sca.  tplus :  0.72059E-02 0.20711E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27336E+00      10   0.12493E-04   0.44905E+01 0.34545E+02 
c  Velocity[X]                                      0.19220E+01 
c  Velocity[Y]                                      0.12367E+01 
c  Velocity[Z]                                      0.13318E+01 
c  Pressure     0.16179E-04      16   0.27297E-03   0.16409E-01 0.11268E+02 
c  k            0.19252E-01      12   0.71496E-04   0.14064E+00 0.55786E+02 
c  omega        0.27922E+07       1   0.96226E-07   0.18418E+08 0.71812E+00 
c  TempK        0.10076E+05       5   0.30243E-05   0.61926E+01 0.89020E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3626e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.035          19.127       0.0044286      -0.0075671
v  Velocity[Y]             -15.685          15.417         0.25879         0.36644
v  Velocity[Z]             -25.608          11.926         -1.6432        -0.50677
v  ǁVelocityǁ         0.00033722          25.769          7.6759           6.578
v  Pressure                -542.35          208.49          32.355          37.079
v  k                   9.8463e-011          7.7237         0.22914         0.49477
v  omega                    57.488     2.7318e+008     1.2912e+006           76872
v  TempK                    298.58          363.17          337.42          345.91
v  TurbVisc            2.4674e-018        0.002053     5.7697e-005      0.00020323
v  CourantNb            0.00012259          1.5717         0.79041         0.97144
v  FourierNb             0.0038154               1         0.41658         0.17749
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034592      7.403e-005      0.00020288

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.55
v  Yplus               0          2.9237         0.62955         0.48524


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56954          2.1665           1.207          1.1489


 INSTANT    0.786000000E-02   TIME STEP NUMBER             786
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925645E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15071E-01 0.46668E+01
   Friction velocity        uk    :  0.15071E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10219E-01 0.29237E+01
   Friction thermal sca.    tstar :  0.12149E+01 0.16766E+03
   Rough dim-less th. sca.  tplus :  0.72390E-02 0.20711E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27332E+00      10   0.12624E-04   0.44848E+01 0.34527E+02 
c  Velocity[X]                                      0.19238E+01 
c  Velocity[Y]                                      0.12327E+01 
c  Velocity[Z]                                      0.13283E+01 
c  Pressure     0.15650E-04      16   0.26984E-03   0.15875E-01 0.11147E+02 
c  k            0.19270E-01      12   0.70534E-04   0.14012E+00 0.55626E+02 
c  omega        0.27922E+07       1   0.94604E-07   0.12925E+08 0.63514E+00 
c  TempK        0.10075E+05       5   0.30172E-05   0.61738E+01 0.88942E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3616e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.034          19.129       0.0043574      -0.0077164
v  Velocity[Y]              -15.61          15.419         0.25936         0.36718
v  Velocity[Z]             -25.608          11.932         -1.6432        -0.50679
v  ǁVelocityǁ         0.00033953          25.769          7.6756          6.5771
v  Pressure                -542.97          208.47          32.331          37.062
v  k                   9.8458e-011          7.6545         0.22936         0.49537
v  omega                    57.488     2.7318e+008     1.2912e+006           76872
v  TempK                    298.58          363.17          337.43          345.92
v  TurbVisc            2.4673e-018       0.0020477     5.7767e-005      0.00020348
v  CourantNb            0.00012133          1.5719         0.79039          0.9714
v  FourierNb             0.0038154               1         0.41664         0.17767
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035328     7.4029e-005       0.0002029

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.55
v  Yplus               0          2.9237         0.62954         0.48522


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53262          2.1667           1.207          1.1491


 INSTANT    0.787000000E-02   TIME STEP NUMBER             787
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925752E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15154E-01 0.46668E+01
   Friction velocity        uk    :  0.15154E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10274E-01 0.29236E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.16675E+03
   Rough dim-less th. sca.  tplus :  0.72784E-02 0.20711E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27329E+00      10   0.12795E-04   0.44917E+01 0.34574E+02 
c  Velocity[X]                                      0.19272E+01 
c  Velocity[Y]                                      0.12348E+01 
c  Velocity[Z]                                      0.13297E+01 
c  Pressure     0.15670E-04      16   0.28341E-03   0.15899E-01 0.11409E+02 
c  k            0.19288E-01      12   0.69494E-04   0.13952E+00 0.55448E+02 
c  omega        0.27922E+07       1   0.94383E-07   0.10850E+08 0.60544E+00 
c  TempK        0.10075E+05       5   0.30102E-05   0.61558E+01 0.88871E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3603e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.033          19.131       0.0042887      -0.0078651
v  Velocity[Y]             -15.572          15.421         0.25994         0.36791
v  Velocity[Z]             -25.608          11.938         -1.6431        -0.50681
v  ǁVelocityǁ         0.00034104          25.769          7.6754          6.5763
v  Pressure                 -543.6          208.43          32.301          37.039
v  k                   9.8454e-011          7.5905         0.22957         0.49597
v  omega                    57.488     2.7318e+008     1.2912e+006           76872
v  TempK                    298.58          363.17          337.44          345.93
v  TurbVisc            2.4672e-018       0.0020415     5.7837e-005      0.00020374
v  CourantNb            0.00012094          1.5723         0.79037         0.97137
v  FourierNb             0.0038154               1          0.4167         0.17785
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036031     7.4028e-005      0.00020291

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.55
v  Yplus               0          2.9236         0.62953          0.4852


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59033           2.167          1.2071          1.1492


 INSTANT    0.788000000E-02   TIME STEP NUMBER             788
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925596E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15218E-01 0.46668E+01
   Friction velocity        uk    :  0.15218E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10318E-01 0.29236E+01
   Friction thermal sca.    tstar :  0.12145E+01 0.16605E+03
   Rough dim-less th. sca.  tplus :  0.73094E-02 0.20711E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27325E+00      10   0.12895E-04   0.45015E+01 0.34637E+02 
c  Velocity[X]                                      0.19300E+01 
c  Velocity[Y]                                      0.12395E+01 
c  Velocity[Z]                                      0.13319E+01 
c  Pressure     0.15458E-04      16   0.26385E-03   0.15687E-01 0.11009E+02 
c  k            0.19306E-01      12   0.68841E-04   0.13882E+00 0.55253E+02 
c  omega        0.27922E+07       1   0.96052E-07   0.15684E+08 0.69881E+00 
c  TempK        0.10074E+05       5   0.30031E-05   0.61351E+01 0.88787E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3586e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.032          19.133       0.0042244      -0.0080173
v  Velocity[Y]             -15.588          15.423         0.26051         0.36865
v  Velocity[Z]             -25.607          11.944         -1.6431        -0.50684
v  ǁVelocityǁ         0.00034321          25.769          7.6752          6.5754
v  Pressure                -544.23           208.4          32.276          37.022
v  k                   9.8449e-011           7.531         0.22978         0.49656
v  omega                    57.488     2.7318e+008     1.2912e+006           76871
v  TempK                    298.58          363.17          337.44          345.95
v  TurbVisc            2.4671e-018       0.0020343     5.7907e-005        0.000204
v  CourantNb             0.0001218          1.5727         0.79035         0.97133
v  FourierNb             0.0038154               1         0.41676         0.17804
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036673     7.4028e-005      0.00020292

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.55
v  Yplus               0          2.9236         0.62952         0.48518


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49886          2.1674          1.2071          1.1494


 INSTANT    0.789000000E-02   TIME STEP NUMBER             789
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925742E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15283E-01 0.46668E+01
   Friction velocity        uk    :  0.15282E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10362E-01 0.29235E+01
   Friction thermal sca.    tstar :  0.12145E+01 0.16534E+03
   Rough dim-less th. sca.  tplus :  0.73404E-02 0.20711E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27321E+00      10   0.12884E-04   0.45082E+01 0.34665E+02 
c  Velocity[X]                                      0.19332E+01 
c  Velocity[Y]                                      0.12396E+01 
c  Velocity[Z]                                      0.13354E+01 
c  Pressure     0.15433E-04      16   0.26564E-03   0.15664E-01 0.11984E+02 
c  k            0.19325E-01      12   0.67802E-04   0.13811E+00 0.55050E+02 
c  omega        0.27922E+07       1   0.99228E-07   0.19837E+08 0.76498E+00 
c  TempK        0.10074E+05       5   0.29960E-05   0.61141E+01 0.88695E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3567e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.031          19.135       0.0041606      -0.0081723
v  Velocity[Y]             -15.706          15.424         0.26107         0.36939
v  Velocity[Z]             -25.607           11.95          -1.643        -0.50687
v  ǁVelocityǁ         0.00034543          25.769          7.6749          6.5745
v  Pressure                -544.84          208.36          32.237          36.989
v  k                   9.8445e-011          7.4738            0.23         0.49715
v  omega                    57.489     2.7318e+008     1.2912e+006           76871
v  TempK                    298.57          363.17          337.45          345.96
v  TurbVisc             2.467e-018       0.0020261     5.7977e-005      0.00020425
v  CourantNb            0.00012344          1.5731         0.79033         0.97129
v  FourierNb             0.0038154               1         0.41682         0.17822
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034849     7.4028e-005      0.00020294

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.55
v  Yplus               0          2.9235          0.6295         0.48515


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64795          2.1679          1.2071          1.1495


 INSTANT    0.790000000E-02   TIME STEP NUMBER             790
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925686E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15325E-01 0.46668E+01
   Friction velocity        uk    :  0.15325E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10390E-01 0.29235E+01
   Friction thermal sca.    tstar :  0.12149E+01 0.16489E+03
   Rough dim-less th. sca.  tplus :  0.73606E-02 0.20710E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27317E+00      10   0.12671E-04   0.45129E+01 0.34710E+02 
c  Velocity[X]                                      0.19353E+01 
c  Velocity[Y]                                      0.12450E+01 
c  Velocity[Z]                                      0.13326E+01 
c  Pressure     0.15212E-04      17   0.26818E-03   0.15442E-01 0.11799E+02 
c  k            0.19343E-01      12   0.66756E-04   0.13740E+00 0.54848E+02 
c  omega        0.27922E+07       1   0.95383E-07   0.10883E+08 0.62756E+00 
c  TempK        0.10073E+05       5   0.29886E-05   0.60952E+01 0.88583E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3551e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.03          19.137       0.0040997      -0.0083268
v  Velocity[Y]             -15.693          15.425         0.26164         0.37013
v  Velocity[Z]             -25.607          11.956         -1.6429         -0.5069
v  ǁVelocityǁ         0.00034835          25.768          7.6747          6.5737
v  Pressure                -545.43          208.32            32.2          36.959
v  k                    9.844e-011          7.4178         0.23021         0.49773
v  omega                    57.489     2.7318e+008     1.2912e+006           76871
v  TempK                    298.57          363.17          337.46          345.97
v  TurbVisc            2.4669e-018        0.002017     5.8047e-005      0.00020451
v  CourantNb            0.00012639          1.5735          0.7903         0.97125
v  FourierNb             0.0038155               1         0.41688          0.1784
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035367     7.4029e-005      0.00020296

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.55
v  Yplus               0          2.9235          0.6295         0.48513


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62028          2.1683          1.2072          1.1496


 INSTANT    0.791000000E-02   TIME STEP NUMBER             791
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925499E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15381E-01 0.46668E+01
   Friction velocity        uk    :  0.15381E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10428E-01 0.29235E+01
   Friction thermal sca.    tstar :  0.12150E+01 0.16429E+03
   Rough dim-less th. sca.  tplus :  0.73874E-02 0.20710E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27313E+00      10   0.12689E-04   0.45201E+01 0.34726E+02 
c  Velocity[X]                                      0.19411E+01 
c  Velocity[Y]                                      0.12450E+01 
c  Velocity[Z]                                      0.13341E+01 
c  Pressure     0.15445E-04      16   0.27143E-03   0.15681E-01 0.11854E+02 
c  k            0.19361E-01      12   0.65611E-04   0.13664E+00 0.54644E+02 
c  omega        0.27922E+07       1   0.95177E-07   0.11600E+08 0.63806E+00 
c  TempK        0.10073E+05       5   0.29814E-05   0.60739E+01 0.88473E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3542e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.029          19.138       0.0040396      -0.0084776
v  Velocity[Y]             -15.648          15.426          0.2622         0.37087
v  Velocity[Z]             -25.606          11.961         -1.6429        -0.50693
v  ǁVelocityǁ         0.00035173          25.768          7.6744          6.5728
v  Pressure                -546.02          208.27           32.16          36.927
v  k                   9.8435e-011           7.361         0.23043         0.49831
v  omega                    57.489     2.7318e+008     1.2912e+006           76870
v  TempK                    298.57          363.17          337.47          345.98
v  TurbVisc            2.4668e-018       0.0020069     5.8116e-005      0.00020475
v  CourantNb             0.0001303          1.5738         0.79028         0.97121
v  FourierNb             0.0038155               1         0.41694         0.17858
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035968     7.4031e-005      0.00020297

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.55
v  Yplus               0          2.9235         0.62948         0.48511


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65508          2.1686          1.2072          1.1498


 INSTANT    0.792000000E-02   TIME STEP NUMBER             792
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925578E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15461E-01 0.46668E+01
   Friction velocity        uk    :  0.15461E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10483E-01 0.29234E+01
   Friction thermal sca.    tstar :  0.12147E+01 0.16343E+03
   Rough dim-less th. sca.  tplus :  0.74262E-02 0.20710E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27310E+00      10   0.12716E-04   0.45295E+01 0.34754E+02 
c  Velocity[X]                                      0.19462E+01 
c  Velocity[Y]                                      0.12456E+01 
c  Velocity[Z]                                      0.13376E+01 
c  Pressure     0.15413E-04      17   0.26492E-03   0.15651E-01 0.12153E+02 
c  k            0.19379E-01      12   0.64722E-04   0.13591E+00 0.54434E+02 
c  omega        0.27922E+07       1   0.96284E-07   0.17836E+08 0.73458E+00 
c  TempK        0.10072E+05       5   0.29741E-05   0.60497E+01 0.88336E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3535e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.028           19.14       0.0039816      -0.0086282
v  Velocity[Y]             -15.561          15.428         0.26276         0.37162
v  Velocity[Z]             -25.606          11.967         -1.6428        -0.50695
v  ǁVelocityǁ         0.00035504          25.767          7.6742           6.572
v  Pressure                -546.61          208.23          32.119          36.893
v  k                   9.8431e-011          7.3028         0.23064         0.49889
v  omega                    57.489     2.7318e+008     1.2912e+006           76870
v  TempK                    298.57          363.17          337.47             346
v  TurbVisc            2.4666e-018       0.0019958     5.8185e-005        0.000205
v  CourantNb            0.00013545          1.5739         0.79026         0.97118
v  FourierNb             0.0038155               1           0.417         0.17876
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036614     7.4032e-005      0.00020299

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.55
v  Yplus               0          2.9234         0.62947         0.48509


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5656          2.1688          1.2073          1.1499


 INSTANT    0.793000000E-02   TIME STEP NUMBER             793
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925549E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15541E-01 0.46668E+01
   Friction velocity        uk    :  0.15541E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10537E-01 0.29234E+01
   Friction thermal sca.    tstar :  0.12145E+01 0.16260E+03
   Rough dim-less th. sca.  tplus :  0.74645E-02 0.20709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27306E+00      10   0.12765E-04   0.45384E+01 0.34776E+02 
c  Velocity[X]                                      0.19522E+01 
c  Velocity[Y]                                      0.12460E+01 
c  Velocity[Z]                                      0.13402E+01 
c  Pressure     0.15378E-04      17   0.25934E-03   0.15619E-01 0.12023E+02 
c  k            0.19397E-01      12   0.63659E-04   0.13518E+00 0.54223E+02 
c  omega        0.27922E+07       1   0.93251E-07   0.84075E+07 0.57037E+00 
c  TempK        0.10072E+05       5   0.29666E-05   0.60268E+01 0.88205E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3525e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.027          19.142       0.0039266      -0.0087799
v  Velocity[Y]             -15.517           15.43         0.26332         0.37236
v  Velocity[Z]             -25.605          11.972         -1.6427        -0.50698
v  ǁVelocityǁ         0.00035954          25.767          7.6739          6.5711
v  Pressure                -547.18          208.18          32.077          36.858
v  k                   9.8426e-011          7.2422         0.23086         0.49947
v  omega                    57.489     2.7318e+008     1.2912e+006           76870
v  TempK                    298.56          363.17          337.48          346.01
v  TurbVisc            2.4665e-018       0.0019874     5.8253e-005      0.00020525
v  CourantNb            0.00014158          1.5742         0.79024         0.97115
v  FourierNb             0.0038155               1         0.41706         0.17894
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036916     7.4034e-005      0.00020302

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.55
v  Yplus               0          2.9234         0.62945         0.48507


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59528           2.169          1.2073          1.1501


 INSTANT    0.794000000E-02   TIME STEP NUMBER             794
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925651E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15614E-01 0.46668E+01
   Friction velocity        uk    :  0.15614E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10587E-01 0.29233E+01
   Friction thermal sca.    tstar :  0.12145E+01 0.16183E+03
   Rough dim-less th. sca.  tplus :  0.74997E-02 0.20709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27302E+00      10   0.12755E-04   0.45459E+01 0.34815E+02 
c  Velocity[X]                                      0.19573E+01 
c  Velocity[Y]                                      0.12480E+01 
c  Velocity[Z]                                      0.13406E+01 
c  Pressure     0.15375E-04      17   0.26136E-03   0.15618E-01 0.12277E+02 
c  k            0.19416E-01      12   0.62641E-04   0.13439E+00 0.54007E+02 
c  omega        0.27922E+07       1   0.93376E-07   0.94521E+07 0.58304E+00 
c  TempK        0.10071E+05       5   0.29592E-05   0.60045E+01 0.88081E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.351e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.025          19.144       0.0038719      -0.0089322
v  Velocity[Y]             -15.519          15.431         0.26388         0.37311
v  Velocity[Z]             -25.605          11.977         -1.6426        -0.50701
v  ǁVelocityǁ         0.00036378          25.766          7.6737          6.5702
v  Pressure                -547.75          208.14          32.033          36.822
v  k                   9.8421e-011          7.1784         0.23107         0.50005
v  omega                     57.49     2.7318e+008     1.2912e+006           76870
v  TempK                    298.56          363.17          337.49          346.02
v  TurbVisc            2.4664e-018       0.0019747     5.8322e-005       0.0002055
v  CourantNb            0.00014869          1.5746         0.79022         0.97111
v  FourierNb             0.0038155               1         0.41712         0.17912
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036971     7.4037e-005      0.00020304

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.55
v  Yplus               0          2.9233         0.62944         0.48506


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62111          2.1694          1.2073          1.1502


 INSTANT    0.795000000E-02   TIME STEP NUMBER             795
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925578E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15682E-01 0.46668E+01
   Friction velocity        uk    :  0.15682E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10633E-01 0.29233E+01
   Friction thermal sca.    tstar :  0.12145E+01 0.16113E+03
   Rough dim-less th. sca.  tplus :  0.75323E-02 0.20709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27298E+00      10   0.12782E-04   0.45545E+01 0.34887E+02 
c  Velocity[X]                                      0.19601E+01 
c  Velocity[Y]                                      0.12508E+01 
c  Velocity[Z]                                      0.13435E+01 
c  Pressure     0.15300E-04      17   0.26540E-03   0.15543E-01 0.12296E+02 
c  k            0.19434E-01      12   0.61709E-04   0.13355E+00 0.53792E+02 
c  omega        0.27922E+07       1   0.95118E-07   0.13627E+08 0.64963E+00 
c  TempK        0.10070E+05       5   0.29519E-05   0.59838E+01 0.87956E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3493e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.024          19.146        0.003816      -0.0090871
v  Velocity[Y]             -15.609          15.433         0.26444         0.37386
v  Velocity[Z]             -25.604          11.982         -1.6426        -0.50703
v  ǁVelocityǁ         0.00036885          25.765          7.6735          6.5694
v  Pressure                 -548.3          208.09          31.991          36.786
v  k                   9.8416e-011          7.1109         0.23129         0.50062
v  omega                     57.49     2.7318e+008     1.2912e+006           76869
v  TempK                    298.56          363.17          337.49          346.03
v  TurbVisc            2.4663e-018       0.0019578      5.839e-005      0.00020574
v  CourantNb            0.00015679           1.575          0.7902         0.97109
v  FourierNb             0.0038155               1         0.41718          0.1793
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036897      7.404e-005      0.00020306

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.55
v  Yplus               0          2.9233         0.62943         0.48504


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54696          2.1698          1.2074          1.1504


 INSTANT    0.796000000E-02   TIME STEP NUMBER             796
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925601E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15736E-01 0.46668E+01
   Friction velocity        uk    :  0.15736E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10669E-01 0.29232E+01
   Friction thermal sca.    tstar :  0.12148E+01 0.16058E+03
   Rough dim-less th. sca.  tplus :  0.75583E-02 0.20708E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27294E+00      10   0.12812E-04   0.45685E+01 0.34961E+02 
c  Velocity[X]                                      0.19664E+01 
c  Velocity[Y]                                      0.12536E+01 
c  Velocity[Z]                                      0.13485E+01 
c  Pressure     0.15234E-04      17   0.26138E-03   0.15477E-01 0.12851E+02 
c  k            0.19453E-01      12   0.60647E-04   0.13269E+00 0.53578E+02 
c  omega        0.27922E+07       1   0.99171E-07   0.26949E+08 0.84262E+00 
c  TempK        0.10070E+05       5   0.29445E-05   0.59657E+01 0.87841E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3476e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.023          19.148       0.0037608      -0.0092426
v  Velocity[Y]             -15.661          15.434         0.26499         0.37461
v  Velocity[Z]             -25.603          11.987         -1.6425        -0.50706
v  ǁVelocityǁ         0.00024819          25.764          7.6732          6.5685
v  Pressure                -548.84          208.04          31.942          36.744
v  k                   9.8411e-011          7.0397          0.2315         0.50119
v  omega                     57.49     2.7318e+008     1.2912e+006           76869
v  TempK                    298.56          363.17           337.5          346.05
v  TurbVisc            2.4662e-018       0.0019494     5.8458e-005      0.00020599
v  CourantNb            0.00016609          1.5754         0.79018         0.97106
v  FourierNb             0.0038154               1         0.41724         0.17948
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036781     7.4042e-005      0.00020308

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.55
v  Yplus               0          2.9232         0.62942         0.48502


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52414          2.1702          1.2074          1.1505


 INSTANT    0.797000000E-02   TIME STEP NUMBER             797
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925611E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15798E-01 0.46668E+01
   Friction velocity        uk    :  0.15798E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10711E-01 0.29231E+01
   Friction thermal sca.    tstar :  0.12149E+01 0.15995E+03
   Rough dim-less th. sca.  tplus :  0.75877E-02 0.20707E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27290E+00      10   0.12903E-04   0.45801E+01 0.35013E+02 
c  Velocity[X]                                      0.19702E+01 
c  Velocity[Y]                                      0.12564E+01 
c  Velocity[Z]                                      0.13535E+01 
c  Pressure     0.15303E-04      18   0.26395E-03   0.15549E-01 0.14418E+02 
c  k            0.19471E-01      12   0.59518E-04   0.13185E+00 0.53375E+02 
c  omega        0.27922E+07       1   0.96053E-07   0.19158E+08 0.73210E+00 
c  TempK        0.10069E+05       5   0.29371E-05   0.59494E+01 0.87709E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3467e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.022           19.15       0.0037051      -0.0093953
v  Velocity[Y]             -15.588          15.435         0.26555         0.37536
v  Velocity[Z]             -25.601          11.991         -1.6424        -0.50708
v  ǁVelocityǁ         0.00038025          25.763           7.673          6.5676
v  Pressure                -549.39          207.97          31.878          36.687
v  k                   9.8406e-011           7.013         0.23172         0.50176
v  omega                     57.49     2.7318e+008     1.2912e+006           76869
v  TempK                    298.56          363.17          337.51          346.06
v  TurbVisc             2.466e-018       0.0019477     5.8527e-005      0.00020623
v  CourantNb            0.00017634          1.5756         0.79016         0.97103
v  FourierNb             0.0038154               1          0.4173         0.17966
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036693     7.4044e-005       0.0002031

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.56
v  Yplus               0          2.9231         0.62941         0.48499


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66244          2.1704          1.2075          1.1507


 INSTANT    0.798000000E-02   TIME STEP NUMBER             798
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925351E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15882E-01 0.46668E+01
   Friction velocity        uk    :  0.15882E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10768E-01 0.29230E+01
   Friction thermal sca.    tstar :  0.12147E+01 0.15911E+03
   Rough dim-less th. sca.  tplus :  0.76282E-02 0.20707E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27285E+00      10   0.12885E-04   0.45820E+01 0.35003E+02 
c  Velocity[X]                                      0.19762E+01 
c  Velocity[Y]                                      0.12503E+01 
c  Velocity[Z]                                      0.13555E+01 
c  Pressure     0.15408E-04      17   0.26608E-03   0.15659E-01 0.13712E+02 
c  k            0.19490E-01      12   0.58644E-04   0.13091E+00 0.53164E+02 
c  omega        0.27922E+07       1   0.92590E-07   0.87812E+07 0.55003E+00 
c  TempK        0.10068E+05       5   0.29300E-05   0.59363E+01 0.87608E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.346e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.021          19.152       0.0036491      -0.0095463
v  Velocity[Y]             -15.527          15.437         0.26611         0.37612
v  Velocity[Z]               -25.6          11.994         -1.6423        -0.50711
v  ǁVelocityǁ         0.00038669          25.762          7.6727          6.5668
v  Pressure                -549.93          207.91          31.822          36.639
v  k                   9.8401e-011          7.0109         0.23193         0.50232
v  omega                     57.49     2.7318e+008     1.2912e+006           76869
v  TempK                    298.56          363.17          337.52          346.07
v  TurbVisc            2.4659e-018       0.0019456     5.8594e-005      0.00020648
v  CourantNb            0.00018743          1.5758         0.79014           0.971
v  FourierNb             0.0038154               1         0.41736         0.17983
v  total_pressure      1.0078e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036675     7.4046e-005      0.00020312

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.56
v  Yplus               0           2.923          0.6294         0.48497


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53721          2.1706          1.2075          1.1508


 INSTANT    0.799000000E-02   TIME STEP NUMBER             799
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925344E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15969E-01 0.46668E+01
   Friction velocity        uk    :  0.15969E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10827E-01 0.29229E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.15824E+03
   Rough dim-less th. sca.  tplus :  0.76699E-02 0.20706E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27281E+00      10   0.12902E-04   0.45915E+01 0.35060E+02 
c  Velocity[X]                                      0.19816E+01 
c  Velocity[Y]                                      0.12500E+01 
c  Velocity[Z]                                      0.13599E+01 
c  Pressure     0.15457E-04      18   0.26576E-03   0.15711E-01 0.14328E+02 
c  k            0.19508E-01      12   0.57675E-04   0.12990E+00 0.52950E+02 
c  omega        0.27922E+07       1   0.92848E-07   0.85183E+07 0.55030E+00 
c  TempK        0.10068E+05       5   0.29225E-05   0.59210E+01 0.87507E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3449e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.02          19.154       0.0035912      -0.0096963
v  Velocity[Y]             -15.514          15.438         0.26668         0.37688
v  Velocity[Z]             -25.599          11.998         -1.6422        -0.50714
v  ǁVelocityǁ         0.00039292          25.761          7.6725          6.5659
v  Pressure                -550.47          207.85          31.761          36.585
v  k                   9.8396e-011          7.0095         0.23215         0.50288
v  omega                    57.491     2.7318e+008     1.2912e+006           76868
v  TempK                    298.55          363.17          337.52          346.08
v  TurbVisc            2.4658e-018       0.0019429     5.8662e-005      0.00020672
v  CourantNb            0.00019582          1.5761         0.79012         0.97098
v  FourierNb             0.0038154               1         0.41742         0.18001
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036719     7.4049e-005      0.00020314

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.56
v  Yplus               0          2.9229         0.62939         0.48495


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52528          2.1709          1.2075           1.151


 INSTANT    0.800000000E-02   TIME STEP NUMBER             800
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925306E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16040E-01 0.46669E+01
   Friction velocity        uk    :  0.16040E-01 0.46629E+01
   Dimensionless distance   yplus :  0.10875E-01 0.29228E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.15754E+03
   Rough dim-less th. sca.  tplus :  0.77042E-02 0.20705E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27277E+00      10   0.12944E-04   0.45942E+01 0.35099E+02 
c  Velocity[X]                                      0.19852E+01 
c  Velocity[Y]                                      0.12486E+01 
c  Velocity[Z]                                      0.13604E+01 
c  Pressure     0.15429E-04      18   0.26593E-03   0.15685E-01 0.14508E+02 
c  k            0.19527E-01      12   0.56829E-04   0.12894E+00 0.52744E+02 
c  omega        0.27922E+07       1   0.94178E-07   0.10971E+08 0.59914E+00 
c  TempK        0.10067E+05       5   0.29152E-05   0.59083E+01 0.87423E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3436e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.019          19.157       0.0035328      -0.0098444
v  Velocity[Y]             -15.565           15.44         0.26723         0.37764
v  Velocity[Z]             -25.597          12.001         -1.6421        -0.50717
v  ǁVelocityǁ          0.0003986          25.759          7.6723           6.565
v  Pressure                -550.98          207.79          31.701          36.532
v  k                   9.8391e-011          7.0087         0.23236         0.50344
v  omega                    57.491     2.7318e+008     1.2912e+006           76868
v  TempK                    298.55          363.17          337.53           346.1
v  TurbVisc            2.4657e-018         0.00194     5.8729e-005      0.00020696
v  CourantNb             0.0001907          1.5764          0.7901         0.97095
v  FourierNb             0.0038154               1         0.41749         0.18019
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036819     7.4051e-005      0.00020317

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.56
v  Yplus               0          2.9228         0.62938         0.48494


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57843          2.1712          1.2076          1.1511


 INSTANT    0.801000000E-02   TIME STEP NUMBER             801
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925408E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16107E-01 0.46669E+01
   Friction velocity        uk    :  0.16107E-01 0.46630E+01
   Dimensionless distance   yplus :  0.10921E-01 0.29227E+01
   Friction thermal sca.    tstar :  0.12146E+01 0.15688E+03
   Rough dim-less th. sca.  tplus :  0.77362E-02 0.20705E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27273E+00      10   0.13089E-04   0.46040E+01 0.35167E+02 
c  Velocity[X]                                      0.19912E+01 
c  Velocity[Y]                                      0.12491E+01 
c  Velocity[Z]                                      0.13637E+01 
c  Pressure     0.15590E-04      18   0.27474E-03   0.15851E-01 0.14913E+02 
c  k            0.19546E-01      12   0.56018E-04   0.12800E+00 0.52544E+02 
c  omega        0.27922E+07       1   0.96991E-07   0.16431E+08 0.69508E+00 
c  TempK        0.10066E+05       5   0.29079E-05   0.58936E+01 0.87342E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.342e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.018          19.161       0.0034735      -0.0099898
v  Velocity[Y]             -15.638          15.441         0.26779          0.3784
v  Velocity[Z]             -25.596          12.004          -1.642         -0.5072
v  ǁVelocityǁ         0.00040619          25.758           7.672          6.5642
v  Pressure                -551.49          207.72          31.638          36.476
v  k                   9.8385e-011          7.0085         0.23257           0.504
v  omega                    57.491     2.7318e+008     1.2912e+006           76868
v  TempK                    298.55          363.17          337.54          346.11
v  TurbVisc            2.4655e-018       0.0019367     5.8796e-005       0.0002072
v  CourantNb            0.00018572          1.5768         0.79008         0.97092
v  FourierNb             0.0038154               1         0.41755         0.18037
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036984     7.4053e-005      0.00020319

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.46          306.56
v  Yplus               0          2.9227         0.62938         0.48492


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.3799          2.1716          1.2076          1.1513


 INSTANT    0.802000000E-02   TIME STEP NUMBER             802
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925319E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16151E-01 0.46669E+01
   Friction velocity        uk    :  0.16151E-01 0.46630E+01
   Dimensionless distance   yplus :  0.10951E-01 0.29226E+01
   Friction thermal sca.    tstar :  0.12150E+01 0.15645E+03
   Rough dim-less th. sca.  tplus :  0.77577E-02 0.20704E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27269E+00      10   0.13157E-04   0.46148E+01 0.35251E+02 
c  Velocity[X]                                      0.19958E+01 
c  Velocity[Y]                                      0.12508E+01 
c  Velocity[Z]                                      0.13682E+01 
c  Pressure     0.15850E-04      18   0.28159E-03   0.16117E-01 0.14451E+02 
c  k            0.19565E-01      12   0.55151E-04   0.12706E+00 0.52350E+02 
c  omega        0.27922E+07       1   0.99400E-07   0.22633E+08 0.79446E+00 
c  TempK        0.10066E+05       5   0.29004E-05   0.58771E+01 0.87262E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3413e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.018          19.164       0.0034114       -0.010135
v  Velocity[Y]             -15.609          15.442         0.26834         0.37916
v  Velocity[Z]             -25.594          12.007         -1.6419        -0.50723
v  ǁVelocityǁ         0.00041234          25.756          7.6718          6.5633
v  Pressure                -551.99          207.66          31.581          36.426
v  k                    9.838e-011           7.009         0.23279         0.50456
v  omega                    57.491     2.7318e+008     1.2912e+006           76867
v  TempK                    298.55          363.17          337.54          346.12
v  TurbVisc            2.4654e-018       0.0019271     5.8863e-005      0.00020745
v  CourantNb            0.00018077           1.577         0.79006          0.9709
v  FourierNb             0.0038154               1         0.41761         0.18054
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037222     7.4055e-005      0.00020321

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.47          306.56
v  Yplus               0          2.9226         0.62938          0.4849


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48054          2.1718          1.2077          1.1514


 INSTANT    0.803000000E-02   TIME STEP NUMBER             803
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925419E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16237E-01 0.46669E+01
   Friction velocity        uk    :  0.16237E-01 0.46630E+01
   Dimensionless distance   yplus :  0.11009E-01 0.29225E+01
   Friction thermal sca.    tstar :  0.12148E+01 0.15562E+03
   Rough dim-less th. sca.  tplus :  0.77988E-02 0.20703E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27265E+00      10   0.13094E-04   0.46195E+01 0.35279E+02 
c  Velocity[X]                                      0.20001E+01 
c  Velocity[Y]                                      0.12484E+01 
c  Velocity[Z]                                      0.13710E+01 
c  Pressure     0.15762E-04      18   0.27976E-03   0.16029E-01 0.16271E+02 
c  k            0.19584E-01      12   0.54318E-04   0.12611E+00 0.52151E+02 
c  omega        0.27922E+07       1   0.98189E-07   0.19057E+08 0.74827E+00 
c  TempK        0.10065E+05       5   0.28930E-05   0.58586E+01 0.87146E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3409e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.017          19.167       0.0033509       -0.010276
v  Velocity[Y]             -15.505          15.443         0.26889         0.37993
v  Velocity[Z]             -25.592          12.009         -1.6418        -0.50726
v  ǁVelocityǁ         0.00040802          25.754          7.6715          6.5625
v  Pressure                 -552.5          207.58          31.505          36.357
v  k                   9.8375e-011          7.0102           0.233         0.50511
v  omega                    57.491     2.7318e+008     1.2912e+006           76867
v  TempK                    298.55          363.17          337.55          346.13
v  TurbVisc            2.4653e-018       0.0019144     5.8929e-005      0.00020769
v  CourantNb            0.00016421          1.5771         0.79004         0.97087
v  FourierNb             0.0038154               1         0.41766         0.18072
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037556     7.4057e-005      0.00020323

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.47          306.56
v  Yplus               0          2.9225         0.62937         0.48489


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69593          2.1719          1.2077          1.1516


 INSTANT    0.804000000E-02   TIME STEP NUMBER             804
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925307E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16328E-01 0.46669E+01
   Friction velocity        uk    :  0.16328E-01 0.46630E+01
   Dimensionless distance   yplus :  0.11070E-01 0.29224E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.15476E+03
   Rough dim-less th. sca.  tplus :  0.78423E-02 0.20702E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27261E+00      10   0.13160E-04   0.46136E+01 0.35255E+02 
c  Velocity[X]                                      0.20049E+01 
c  Velocity[Y]                                      0.12423E+01 
c  Velocity[Z]                                      0.13664E+01 
c  Pressure     0.15971E-04      18   0.27747E-03   0.16244E-01 0.15985E+02 
c  k            0.19603E-01      12   0.53852E-04   0.12521E+00 0.51962E+02 
c  omega        0.27922E+07       1   0.95420E-07   0.99612E+07 0.60901E+00 
c  TempK        0.10065E+05       5   0.28857E-05   0.58434E+01 0.87051E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3401e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.016           19.17       0.0032926       -0.010414
v  Velocity[Y]             -15.469          15.445         0.26945         0.38069
v  Velocity[Z]              -25.59          12.012         -1.6417        -0.50729
v  ǁVelocityǁ         0.00040371          25.752          7.6712          6.5616
v  Pressure                -553.01           207.5          31.432          36.291
v  k                   9.8369e-011          7.0121         0.23321         0.50566
v  omega                    57.492     2.7317e+008     1.2912e+006           76867
v  TempK                    298.55          363.17          337.56          346.15
v  TurbVisc            2.4651e-018       0.0019021     5.8996e-005      0.00020793
v  CourantNb            0.00016054          1.5773         0.79002         0.97084
v  FourierNb             0.0038154               1         0.41772          0.1809
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.003827     7.4059e-005      0.00020325

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.47          306.56
v  Yplus               0          2.9224         0.62936         0.48487


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58389          2.1721          1.2077          1.1517


 INSTANT    0.805000000E-02   TIME STEP NUMBER             805
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925470E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16409E-01 0.46669E+01
   Friction velocity        uk    :  0.16409E-01 0.46630E+01
   Dimensionless distance   yplus :  0.11125E-01 0.29222E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.15399E+03
   Rough dim-less th. sca.  tplus :  0.78813E-02 0.20701E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27256E+00      10   0.13237E-04   0.46238E+01 0.35287E+02 
c  Velocity[X]                                      0.20116E+01 
c  Velocity[Y]                                      0.12387E+01 
c  Velocity[Z]                                      0.13735E+01 
c  Pressure     0.16669E-04      18   0.27421E-03   0.16955E-01 0.16766E+02 
c  k            0.19622E-01      12   0.53106E-04   0.12432E+00 0.51776E+02 
c  omega        0.27922E+07       1   0.95442E-07   0.94620E+07 0.60769E+00 
c  TempK        0.10064E+05       5   0.28785E-05   0.58289E+01 0.86962E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.339e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.015          19.173        0.003231       -0.010548
v  Velocity[Y]             -15.495          15.446            0.27         0.38146
v  Velocity[Z]             -25.588          12.014         -1.6416        -0.50732
v  ǁVelocityǁ         0.00039904           25.75           7.671          6.5608
v  Pressure                -553.51          207.42          31.352          36.218
v  k                   9.8363e-011          7.0145         0.23342         0.50621
v  omega                    57.492     2.7317e+008     1.2912e+006           76867
v  TempK                    298.56          363.17          337.56          346.16
v  TurbVisc             2.465e-018       0.0018904     5.9063e-005      0.00020817
v  CourantNb            0.00016253          1.5775            0.79         0.97081
v  FourierNb             0.0038154               1         0.41779         0.18107
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0040592     7.4062e-005      0.00020327

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.47          306.56
v  Yplus               0          2.9222         0.62936         0.48485


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.32718          2.1724          1.2078          1.1519


 INSTANT    0.806000000E-02   TIME STEP NUMBER             806
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925293E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16480E-01 0.46669E+01
   Friction velocity        uk    :  0.16480E-01 0.46630E+01
   Dimensionless distance   yplus :  0.11174E-01 0.29221E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.15332E+03
   Rough dim-less th. sca.  tplus :  0.79157E-02 0.20700E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27252E+00      10   0.13308E-04   0.46334E+01 0.35342E+02 
c  Velocity[X]                                      0.20171E+01 
c  Velocity[Y]                                      0.12357E+01 
c  Velocity[Z]                                      0.13807E+01 
c  Pressure     0.16597E-04      18   0.27556E-03   0.16884E-01 0.15794E+02 
c  k            0.19642E-01      12   0.52371E-04   0.12350E+00 0.51601E+02 
c  omega        0.27922E+07       1   0.10002E-06   0.18567E+08 0.75949E+00 
c  TempK        0.10063E+05       5   0.28713E-05   0.58143E+01 0.86893E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3375e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.014          19.176       0.0031674       -0.010681
v  Velocity[Y]             -15.654          15.447         0.27053         0.38223
v  Velocity[Z]             -25.586          12.016         -1.6415        -0.50735
v  ǁVelocityǁ         0.00039441          25.748          7.6707          6.5599
v  Pressure                -553.97          207.34          31.282          36.154
v  k                   9.8358e-011          7.0171         0.23363         0.50676
v  omega                    57.492     2.7317e+008     1.2912e+006           76866
v  TempK                    298.56          363.17          337.57          346.17
v  TurbVisc            2.4648e-018       0.0018793     5.9129e-005       0.0002084
v  CourantNb            0.00016217          1.5779         0.78998         0.97078
v  FourierNb             0.0038154               1         0.41784         0.18125
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0043319     7.4063e-005      0.00020329

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.47          306.56
v  Yplus               0          2.9221         0.62936         0.48483


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59859          2.1728          1.2078           1.152


 INSTANT    0.807000000E-02   TIME STEP NUMBER             807
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925361E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16528E-01 0.46669E+01
   Friction velocity        uk    :  0.16528E-01 0.46630E+01
   Dimensionless distance   yplus :  0.11206E-01 0.29220E+01
   Friction thermal sca.    tstar :  0.12148E+01 0.15288E+03
   Rough dim-less th. sca.  tplus :  0.79387E-02 0.20699E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27248E+00      10   0.13339E-04   0.46316E+01 0.35396E+02 
c  Velocity[X]                                      0.20218E+01 
c  Velocity[Y]                                      0.12389E+01 
c  Velocity[Z]                                      0.13709E+01 
c  Pressure     0.16195E-04      18   0.27658E-03   0.16477E-01 0.16733E+02 
c  k            0.19661E-01      12   0.52183E-04   0.12274E+00 0.51437E+02 
c  omega        0.27922E+07       1   0.97811E-07   0.13972E+08 0.69731E+00 
c  TempK        0.10063E+05       5   0.28639E-05   0.57994E+01 0.86795E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3368e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.014          19.179       0.0031041       -0.010808
v  Velocity[Y]             -15.615          15.448         0.27106           0.383
v  Velocity[Z]             -25.584          12.017         -1.6414        -0.50738
v  ǁVelocityǁ         0.00038971          25.746          7.6704          6.5591
v  Pressure                -554.42          207.26          31.201          36.081
v  k                   9.8352e-011          7.0198         0.23384         0.50731
v  omega                    57.492     2.7317e+008     1.2912e+006           76866
v  TempK                    298.56          363.17          337.58          346.18
v  TurbVisc            2.4647e-018       0.0018686     5.9195e-005      0.00020864
v  CourantNb            0.00015773          1.5781         0.78995         0.97075
v  FourierNb             0.0038154               1         0.41791         0.18142
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038305     7.4065e-005      0.00020331

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.47          306.56
v  Yplus               0           2.922         0.62935         0.48482


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5864          2.1729          1.2079          1.1522


 INSTANT    0.808000000E-02   TIME STEP NUMBER             808
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925223E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16600E-01 0.46670E+01
   Friction velocity        uk    :  0.16600E-01 0.46631E+01
   Dimensionless distance   yplus :  0.11255E-01 0.29218E+01
   Friction thermal sca.    tstar :  0.12148E+01 0.15222E+03
   Rough dim-less th. sca.  tplus :  0.79730E-02 0.20699E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27244E+00      10   0.13403E-04   0.46286E+01 0.35372E+02 
c  Velocity[X]                                      0.20254E+01 
c  Velocity[Y]                                      0.12313E+01 
c  Velocity[Z]                                      0.13719E+01 
c  Pressure     0.16323E-04      18   0.27467E-03   0.16608E-01 0.16512E+02 
c  k            0.19680E-01      12   0.51823E-04   0.12196E+00 0.51268E+02 
c  omega        0.27922E+07       1   0.98164E-07   0.13713E+08 0.69603E+00 
c  TempK        0.10062E+05       5   0.28566E-05   0.57838E+01 0.86709E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3364e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.013          19.182       0.0030403        -0.01093
v  Velocity[Y]             -15.544          15.449         0.27159         0.38377
v  Velocity[Z]             -25.582          12.019         -1.6412        -0.50741
v  ǁVelocityǁ          0.0003856          25.744          7.6702          6.5582
v  Pressure                -554.86          207.17          31.123           36.01
v  k                   9.8346e-011          7.0223         0.23405         0.50785
v  omega                    57.492     2.7317e+008     1.2912e+006           76866
v  TempK                    298.56          363.17          337.58          346.19
v  TurbVisc            2.4646e-018       0.0018598      5.926e-005      0.00020888
v  CourantNb            0.00015328          1.5782         0.78993         0.97072
v  FourierNb             0.0038154               1         0.41797          0.1816
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038345     7.4067e-005      0.00020334

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.47          306.56
v  Yplus               0          2.9218         0.62935          0.4848


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48731           2.173          1.2079          1.1523


 INSTANT    0.809000000E-02   TIME STEP NUMBER             809
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925317E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16699E-01 0.46670E+01
   Friction velocity        uk    :  0.16699E-01 0.46631E+01
   Dimensionless distance   yplus :  0.11322E-01 0.29217E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.15131E+03
   Rough dim-less th. sca.  tplus :  0.80209E-02 0.20698E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27239E+00      10   0.13503E-04   0.46278E+01 0.35382E+02 
c  Velocity[X]                                      0.20280E+01 
c  Velocity[Y]                                      0.12270E+01 
c  Velocity[Z]                                      0.13729E+01 
c  Pressure     0.16042E-04      18   0.28048E-03   0.16325E-01 0.16551E+02 
c  k            0.19699E-01      12   0.51579E-04   0.12127E+00 0.51119E+02 
c  omega        0.27922E+07       1   0.97479E-07   0.11524E+08 0.66264E+00 
c  TempK        0.10061E+05       5   0.28494E-05   0.57690E+01 0.86620E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3358e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.012          19.184       0.0029754       -0.011048
v  Velocity[Y]             -15.505           15.45         0.27212         0.38455
v  Velocity[Z]              -25.58           12.02         -1.6411        -0.50745
v  ǁVelocityǁ          0.0003808          25.742          7.6699          6.5574
v  Pressure                -555.29          207.09          31.045          35.939
v  k                    9.834e-011          7.0247         0.23426         0.50839
v  omega                    57.492     2.7317e+008     1.2912e+006           76865
v  TempK                    298.56          363.17          337.59          346.21
v  TurbVisc            2.4644e-018       0.0018663     5.9326e-005      0.00020912
v  CourantNb            0.00014897          1.5783         0.78991         0.97069
v  FourierNb             0.0038154               1         0.41803         0.18177
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038337      7.407e-005      0.00020336

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.47          306.56
v  Yplus               0          2.9217         0.62934         0.48478


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66537          2.1732          1.2079          1.1525


 INSTANT    0.810000000E-02   TIME STEP NUMBER             810
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925530E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15047E-01 0.46670E+01
   Friction velocity        uk    :  0.15047E-01 0.46631E+01
   Dimensionless distance   yplus :  0.10797E-01 0.29216E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.15056E+03
   Rough dim-less th. sca.  tplus :  0.76487E-02 0.20697E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27235E+00      10   0.13571E-04   0.46331E+01 0.35424E+02 
c  Velocity[X]                                      0.20325E+01 
c  Velocity[Y]                                      0.12262E+01 
c  Velocity[Z]                                      0.13744E+01 
c  Pressure     0.16230E-04      17   0.28482E-03   0.16517E-01 0.17219E+02 
c  k            0.19719E-01      12   0.51569E-04   0.12073E+00 0.50998E+02 
c  omega        0.27922E+07       1   0.97848E-07   0.12802E+08 0.68110E+00 
c  TempK        0.10061E+05       5   0.28419E-05   0.57537E+01 0.86514E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.335e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.012          19.187         0.00291       -0.011166
v  Velocity[Y]             -15.508          15.451         0.27264         0.38533
v  Velocity[Z]             -25.578          12.021          -1.641        -0.50748
v  ǁVelocityǁ         0.00037658           25.74          7.6696          6.5565
v  Pressure                 -555.7             207          30.961          35.862
v  k                   9.8334e-011          7.0268         0.23446         0.50893
v  omega                    57.493     2.7317e+008     1.2912e+006           76865
v  TempK                    298.56          363.17           337.6          346.22
v  TurbVisc            2.4643e-018       0.0018733     5.9391e-005      0.00020936
v  CourantNb            0.00014483          1.5785         0.78989         0.97067
v  FourierNb             0.0038154               1         0.41809         0.18194
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038281     7.4073e-005      0.00020338

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.47          306.56
v  Yplus               0          2.9216         0.62933         0.48475


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59179          2.1734           1.208          1.1526


 INSTANT    0.811000000E-02   TIME STEP NUMBER             811
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925520E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16856E-01 0.46670E+01
   Friction velocity        uk    :  0.16856E-01 0.46631E+01
   Dimensionless distance   yplus :  0.11428E-01 0.29214E+01
   Friction thermal sca.    tstar :  0.12145E+01 0.14991E+03
   Rough dim-less th. sca.  tplus :  0.80959E-02 0.20695E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27231E+00      10   0.13611E-04   0.46387E+01 0.35455E+02 
c  Velocity[X]                                      0.20385E+01 
c  Velocity[Y]                                      0.12235E+01 
c  Velocity[Z]                                      0.13766E+01 
c  Pressure     0.16265E-04      18   0.29302E-03   0.16554E-01 0.17406E+02 
c  k            0.19738E-01      12   0.51597E-04   0.12018E+00 0.50869E+02 
c  omega        0.27922E+07       1   0.98638E-07   0.15099E+08 0.71441E+00 
c  TempK        0.10060E+05       5   0.28343E-05   0.57391E+01 0.86408E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3337e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.011          19.189       0.0028438       -0.011284
v  Velocity[Y]             -15.583          15.453         0.27316         0.38612
v  Velocity[Z]             -25.575          12.022         -1.6409        -0.50752
v  ǁVelocityǁ         0.00037197          25.737          7.6693          6.5557
v  Pressure                -556.09          206.91          30.876          35.783
v  k                   9.8328e-011          7.0287         0.23467         0.50947
v  omega                    57.493     2.7317e+008     1.2912e+006           76865
v  TempK                    298.56          363.17           337.6          346.23
v  TurbVisc            2.4641e-018       0.0018809     5.9455e-005       0.0002096
v  CourantNb            0.00014076          1.5788         0.78987         0.97064
v  FourierNb             0.0038154               1         0.41815         0.18212
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038174     7.4076e-005       0.0002034

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.47          306.56
v  Yplus               0          2.9214         0.62932         0.48473


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61262          2.1737           1.208          1.1528


 INSTANT    0.812000000E-02   TIME STEP NUMBER             812
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925501E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16919E-01 0.46670E+01
   Friction velocity        uk    :  0.16919E-01 0.46631E+01
   Dimensionless distance   yplus :  0.11472E-01 0.29212E+01
   Friction thermal sca.    tstar :  0.12146E+01 0.14934E+03
   Rough dim-less th. sca.  tplus :  0.81266E-02 0.20694E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27227E+00      10   0.13652E-04   0.46491E+01 0.35490E+02 
c  Velocity[X]                                      0.20447E+01 
c  Velocity[Y]                                      0.12234E+01 
c  Velocity[Z]                                      0.13809E+01 
c  Pressure     0.16625E-04      18   0.28999E-03   0.16921E-01 0.18257E+02 
c  k            0.19757E-01      12   0.51575E-04   0.11968E+00 0.50743E+02 
c  omega        0.27922E+07       1   0.99773E-07   0.19661E+08 0.77970E+00 
c  TempK        0.10059E+05       5   0.28270E-05   0.57250E+01 0.86309E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3324e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.011          19.191         0.00278       -0.011399
v  Velocity[Y]             -15.631          15.453         0.27367         0.38691
v  Velocity[Z]             -25.572          12.022         -1.6408        -0.50756
v  ǁVelocityǁ         0.00036772          25.734           7.669          6.5549
v  Pressure                -556.47          206.81          30.785            35.7
v  k                   9.8321e-011          7.0304         0.23487            0.51
v  omega                    57.493     2.7317e+008     1.2912e+006           76865
v  TempK                    298.56          363.17          337.61          346.24
v  TurbVisc             2.464e-018       0.0018887     5.9519e-005      0.00020983
v  CourantNb            0.00013676          1.5792         0.78985         0.97062
v  FourierNb             0.0038154               1         0.41821         0.18229
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038005      7.408e-005      0.00020342

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.47          306.56
v  Yplus               0          2.9212         0.62931         0.48471


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50555           2.174          1.2081          1.1529


 INSTANT    0.813000000E-02   TIME STEP NUMBER             813
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925332E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16947E-01 0.46671E+01
   Friction velocity        uk    :  0.16947E-01 0.46632E+01
   Dimensionless distance   yplus :  0.11490E-01 0.29211E+01
   Friction thermal sca.    tstar :  0.12149E+01 0.14886E+03
   Rough dim-less th. sca.  tplus :  0.81397E-02 0.20693E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27223E+00      10   0.13670E-04   0.46598E+01 0.35533E+02 
c  Velocity[X]                                      0.20525E+01 
c  Velocity[Y]                                      0.12258E+01 
c  Velocity[Z]                                      0.13815E+01 
c  Pressure     0.16459E-04      18   0.29511E-03   0.16751E-01 0.18070E+02 
c  k            0.19776E-01      12   0.51804E-04   0.11929E+00 0.50638E+02 
c  omega        0.27922E+07       1   0.98727E-07   0.17726E+08 0.75264E+00 
c  TempK        0.10059E+05       5   0.28191E-05   0.57033E+01 0.86193E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3319e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.01          19.193       0.0027164       -0.011509
v  Velocity[Y]             -15.564          15.454         0.27418         0.38771
v  Velocity[Z]             -25.569          12.023         -1.6407        -0.50759
v  ǁVelocityǁ         0.00036355          25.732          7.6687          6.5541
v  Pressure                -556.84          206.72          30.696          35.617
v  k                   9.8315e-011          7.0319         0.23507         0.51053
v  omega                    57.493     2.7317e+008     1.2912e+006           76864
v  TempK                    298.56          363.17          337.62          346.25
v  TurbVisc            2.4638e-018       0.0018968     5.9582e-005      0.00021007
v  CourantNb            0.00013287          1.5793         0.78983         0.97059
v  FourierNb             0.0038154               1         0.41826         0.18246
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037744     7.4083e-005      0.00020344

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.47          306.56
v  Yplus               0          2.9211         0.62929         0.48468


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65206          2.1742          1.2081          1.1531


 INSTANT    0.814000000E-02   TIME STEP NUMBER             814
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925286E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16593E-01 0.46671E+01
   Friction velocity        uk    :  0.16593E-01 0.46632E+01
   Dimensionless distance   yplus :  0.11250E-01 0.29209E+01
   Friction thermal sca.    tstar :  0.12147E+01 0.14993E+03
   Rough dim-less th. sca.  tplus :  0.79699E-02 0.20692E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27218E+00      10   0.13680E-04   0.46572E+01 0.35510E+02 
c  Velocity[X]                                      0.20597E+01 
c  Velocity[Y]                                      0.12205E+01 
c  Velocity[Z]                                      0.13770E+01 
c  Pressure     0.16459E-04      18   0.29111E-03   0.16752E-01 0.18432E+02 
c  k            0.19794E-01      12   0.52036E-04   0.11902E+00 0.50557E+02 
c  omega        0.27922E+07       1   0.95803E-07   0.93740E+07 0.61837E+00 
c  TempK        0.10058E+05       5   0.28109E-05   0.56797E+01 0.86085E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3316e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.01          19.195       0.0026527       -0.011612
v  Velocity[Y]             -15.501          15.455         0.27468         0.38851
v  Velocity[Z]             -25.567          12.023         -1.6405        -0.50762
v  ǁVelocityǁ         0.00036001          25.729          7.6684          6.5533
v  Pressure                -557.19          206.62          30.602          35.531
v  k                   9.8309e-011          7.0334         0.23527         0.51106
v  omega                    57.493     2.7317e+008     1.2912e+006           76864
v  TempK                    298.57          363.17          337.62          346.26
v  TurbVisc            2.4636e-018       0.0019072     5.9645e-005       0.0002103
v  CourantNb            0.00012126          1.5794         0.78981         0.97057
v  FourierNb             0.0038154               1         0.41832         0.18262
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037405     7.4086e-005      0.00020346

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.47          306.56
v  Yplus               0          2.9209         0.62928         0.48466


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60948          2.1743          1.2081          1.1532


 INSTANT    0.815000000E-02   TIME STEP NUMBER             815
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925333E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16275E-01 0.46671E+01
   Friction velocity        uk    :  0.16275E-01 0.46632E+01
   Dimensionless distance   yplus :  0.11035E-01 0.29207E+01
   Friction thermal sca.    tstar :  0.12142E+01 0.15286E+03
   Rough dim-less th. sca.  tplus :  0.78170E-02 0.20691E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27214E+00      10   0.13717E-04   0.46671E+01 0.35545E+02 
c  Velocity[X]                                      0.20682E+01 
c  Velocity[Y]                                      0.12201E+01 
c  Velocity[Z]                                      0.13787E+01 
c  Pressure     0.16407E-04      18   0.29298E-03   0.16699E-01 0.18259E+02 
c  k            0.19813E-01      12   0.52523E-04   0.11887E+00 0.50497E+02 
c  omega        0.27922E+07       1   0.95780E-07   0.92937E+07 0.61989E+00 
c  TempK        0.10057E+05       4   0.52679E-05   0.52377E+01 0.82716E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3309e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.01          19.197       0.0025901        -0.01171
v  Velocity[Y]             -15.486          15.456         0.27518         0.38931
v  Velocity[Z]             -25.564          12.025         -1.6404        -0.50765
v  ǁVelocityǁ         0.00035578          25.727          7.6681          6.5525
v  Pressure                -557.51          206.52           30.51          35.446
v  k                   9.8302e-011          7.0348         0.23547         0.51159
v  omega                    57.494     2.7317e+008     1.2912e+006           76864
v  TempK                    298.56          363.17          337.63          346.28
v  TurbVisc            2.4635e-018       0.0019181     5.9707e-005      0.00021053
v  CourantNb           9.6307e-005          1.5796         0.78979         0.97055
v  FourierNb             0.0038154               1         0.41838         0.18279
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037008     7.4089e-005      0.00020348

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.47          306.57
v  Yplus               0          2.9207         0.62927         0.48463


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59036          2.1744          1.2082          1.1533


 INSTANT    0.816000000E-02   TIME STEP NUMBER             816
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925338E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15875E-01 0.46671E+01
   Friction velocity        uk    :  0.15875E-01 0.46632E+01
   Dimensionless distance   yplus :  0.10764E-01 0.29206E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.15671E+03
   Rough dim-less th. sca.  tplus :  0.76251E-02 0.20690E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27210E+00      10   0.13822E-04   0.46780E+01 0.35587E+02 
c  Velocity[X]                                      0.20792E+01 
c  Velocity[Y]                                      0.12191E+01 
c  Velocity[Z]                                      0.13797E+01 
c  Pressure     0.16556E-04      18   0.29196E-03   0.16852E-01 0.18729E+02 
c  k            0.19831E-01      12   0.53025E-04   0.11890E+00 0.50467E+02 
c  omega        0.27922E+07       1   0.96770E-07   0.11576E+08 0.65927E+00 
c  TempK        0.10057E+05       4   0.52571E-05   0.52311E+01 0.82733E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3299e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.009          19.199       0.0025277       -0.011804
v  Velocity[Y]             -15.542          15.457         0.27566         0.39011
v  Velocity[Z]             -25.562          12.028         -1.6403        -0.50768
v  ǁVelocityǁ         0.00035262          25.724          7.6677          6.5517
v  Pressure                -557.82          206.42          30.414          35.356
v  k                   9.8295e-011          7.0362         0.23567         0.51211
v  omega                    57.494     2.7317e+008     1.2912e+006           76863
v  TempK                    298.56          363.17          337.64          346.29
v  TurbVisc            2.4633e-018       0.0019289     5.9768e-005      0.00021076
v  CourantNb           9.4467e-005          1.5798         0.78977         0.97053
v  FourierNb             0.0038154               1         0.41843         0.18295
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036575     7.4092e-005       0.0002035

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.47          306.57
v  Yplus               0          2.9206         0.62926         0.48461


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62861          2.1747          1.2082          1.1535


 INSTANT    0.817000000E-02   TIME STEP NUMBER             817
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925289E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15553E-01 0.46672E+01
   Friction velocity        uk    :  0.15553E-01 0.46632E+01
   Dimensionless distance   yplus :  0.10545E-01 0.29204E+01
   Friction thermal sca.    tstar :  0.12145E+01 0.15995E+03
   Rough dim-less th. sca.  tplus :  0.74704E-02 0.20689E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27206E+00      10   0.13973E-04   0.46915E+01 0.35666E+02 
c  Velocity[X]                                      0.20881E+01 
c  Velocity[Y]                                      0.12198E+01 
c  Velocity[Z]                                      0.13836E+01 
c  Pressure     0.16564E-04      18   0.29296E-03   0.16861E-01 0.17665E+02 
c  k            0.19850E-01      12   0.53584E-04   0.11903E+00 0.50454E+02 
c  omega        0.27922E+07       1   0.10009E-06   0.19108E+08 0.77112E+00 
c  TempK        0.10056E+05       4   0.52461E-05   0.52277E+01 0.82765E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3287e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.009          19.201       0.0024651       -0.011898
v  Velocity[Y]              -15.62          15.458         0.27615         0.39092
v  Velocity[Z]             -25.559           12.03         -1.6402        -0.50772
v  ǁVelocityǁ         0.00034889          25.722          7.6674          6.5509
v  Pressure                -558.09          206.32          30.328          35.276
v  k                   9.8289e-011          7.0376         0.23587         0.51263
v  omega                    57.494     2.7317e+008     1.2912e+006           76863
v  TempK                    298.56          363.17          337.64           346.3
v  TurbVisc            2.4631e-018       0.0019397     5.9829e-005      0.00021099
v  CourantNb           9.2371e-005          1.5801         0.78974         0.97051
v  FourierNb             0.0038155               1         0.41849         0.18311
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0036112     7.4094e-005      0.00020352

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.47          306.57
v  Yplus               0          2.9204         0.62924         0.48458


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62644           2.175          1.2082          1.1536


 INSTANT    0.818000000E-02   TIME STEP NUMBER             818
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925369E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15159E-01 0.46672E+01
   Friction velocity        uk    :  0.15159E-01 0.46633E+01
   Dimensionless distance   yplus :  0.10278E-01 0.29202E+01
   Friction thermal sca.    tstar :  0.12149E+01 0.16411E+03
   Rough dim-less th. sca.  tplus :  0.72812E-02 0.20687E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27202E+00      10   0.14006E-04   0.47072E+01 0.35757E+02 
c  Velocity[X]                                      0.20983E+01 
c  Velocity[Y]                                      0.12260E+01 
c  Velocity[Z]                                      0.13830E+01 
c  Pressure     0.16823E-04      18   0.29432E-03   0.17125E-01 0.19098E+02 
c  k            0.19868E-01      12   0.54210E-04   0.11924E+00 0.50460E+02 
c  omega        0.27922E+07       1   0.10102E-06   0.25725E+08 0.86087E+00 
c  TempK        0.10055E+05       4   0.52346E-05   0.52241E+01 0.82780E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3283e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.009          19.203       0.0024028       -0.011986
v  Velocity[Y]             -15.593          15.458         0.27662         0.39173
v  Velocity[Z]             -25.556          12.032         -1.6401        -0.50775
v  ǁVelocityǁ         0.00034634          25.719          7.6671          6.5502
v  Pressure                -558.36          206.22          30.229          35.184
v  k                   9.8282e-011          7.0389         0.23606         0.51315
v  omega                    57.494     2.7317e+008     1.2912e+006           76863
v  TempK                    298.56          363.17          337.65          346.31
v  TurbVisc             2.463e-018       0.0019507     5.9889e-005      0.00021122
v  CourantNb            0.00011478          1.5802         0.78972         0.97049
v  FourierNb             0.0038155               1         0.41855         0.18327
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035392     7.4097e-005      0.00020354

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.47          306.57
v  Yplus               0          2.9202         0.62923         0.48455


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54465          2.1751          1.2083          1.1538


 INSTANT    0.819000000E-02   TIME STEP NUMBER             819
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925304E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14859E-01 0.46672E+01
   Friction velocity        uk    :  0.14859E-01 0.46633E+01
   Dimensionless distance   yplus :  0.10075E-01 0.29200E+01
   Friction thermal sca.    tstar :  0.12148E+01 0.16743E+03
   Rough dim-less th. sca.  tplus :  0.71370E-02 0.20686E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27197E+00      10   0.14146E-04   0.47081E+01 0.35734E+02 
c  Velocity[X]                                      0.21056E+01 
c  Velocity[Y]                                      0.12200E+01 
c  Velocity[Z]                                      0.13825E+01 
c  Pressure     0.16841E-04      18   0.29141E-03   0.17145E-01 0.20068E+02 
c  k            0.19885E-01      12   0.55080E-04   0.11952E+00 0.50480E+02 
c  omega        0.27922E+07       1   0.97069E-07   0.13854E+08 0.68954E+00 
c  TempK        0.10055E+05       4   0.52224E-05   0.52131E+01 0.82759E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3281e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.009          19.205       0.0023394       -0.012072
v  Velocity[Y]             -15.493          15.459         0.27709         0.39254
v  Velocity[Z]             -25.553          12.034           -1.64        -0.50778
v  ǁVelocityǁ         0.00034311          25.716          7.6667          6.5494
v  Pressure                -558.63          206.11          30.123          35.084
v  k                   9.8275e-011          7.0402         0.23626         0.51366
v  omega                    57.494     2.7317e+008     1.2912e+006           76863
v  TempK                    298.56          363.17          337.66          346.32
v  TurbVisc            2.4628e-018       0.0019617      5.995e-005      0.00021145
v  CourantNb             0.0001166          1.5802          0.7897         0.97047
v  FourierNb             0.0038155               1          0.4186         0.18344
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006       0.0034326     7.4102e-005      0.00020355

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.48          306.57
v  Yplus               0            2.92         0.62921         0.48452


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40155          2.1751          1.2083          1.1539


 INSTANT    0.820000000E-02   TIME STEP NUMBER             820
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925276E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14461E-01 0.46672E+01
   Friction velocity        uk    :  0.14461E-01 0.46633E+01
   Dimensionless distance   yplus :  0.98047E-02 0.29199E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.17204E+03
   Rough dim-less th. sca.  tplus :  0.69457E-02 0.20685E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27193E+00      10   0.14336E-04   0.47122E+01 0.35736E+02 
c  Velocity[X]                                      0.21136E+01 
c  Velocity[Y]                                      0.12157E+01 
c  Velocity[Z]                                      0.13829E+01 
c  Pressure     0.16852E-04      18   0.29580E-03   0.17159E-01 0.20186E+02 
c  k            0.19903E-01      12   0.56091E-04   0.12003E+00 0.50532E+02 
c  omega        0.27922E+07       1   0.95053E-07   0.94530E+07 0.60818E+00 
c  TempK        0.10054E+05       4   0.52103E-05   0.52018E+01 0.82738E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3277e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.009          19.207       0.0022754       -0.012153
v  Velocity[Y]             -15.461           15.46         0.27755         0.39336
v  Velocity[Z]              -25.55          12.035         -1.6398        -0.50782
v  ǁVelocityǁ         0.00034075          25.713          7.6664          6.5486
v  Pressure                -558.87          205.99          30.015          34.984
v  k                   9.8268e-011          7.0413         0.23646         0.51417
v  omega                    57.494     2.7317e+008     1.2912e+006           76862
v  TempK                    298.56          363.17          337.66          346.33
v  TurbVisc            2.4626e-018        0.001973      6.001e-005      0.00021168
v  CourantNb            0.00011953          1.5804         0.78968         0.97045
v  FourierNb             0.0038155               1         0.41866         0.18359
v  total_pressure      1.0077e+005     1.0153e+005     1.0136e+005     1.0136e+005
v  Local Time Step          1e-006        0.003313     7.4106e-005      0.00020357

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.48          306.57
v  Yplus               0          2.9199         0.62919         0.48449


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53753          2.1752          1.2083           1.154


 INSTANT    0.821000000E-02   TIME STEP NUMBER             821
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925337E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14141E-01 0.46673E+01
   Friction velocity        uk    :  0.14141E-01 0.46633E+01
   Dimensionless distance   yplus :  0.95880E-02 0.29197E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.17593E+03
   Rough dim-less th. sca.  tplus :  0.67922E-02 0.20683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27189E+00      10   0.14395E-04   0.47245E+01 0.35776E+02 
c  Velocity[X]                                      0.21235E+01 
c  Velocity[Y]                                      0.12153E+01 
c  Velocity[Z]                                      0.13857E+01 
c  Pressure     0.16917E-04      18   0.30223E-03   0.17228E-01 0.20348E+02 
c  k            0.19920E-01      12   0.57286E-04   0.12082E+00 0.50620E+02 
c  omega        0.27922E+07       1   0.94509E-07   0.85421E+07 0.58399E+00 
c  TempK        0.10054E+05       4   0.51982E-05   0.51908E+01 0.82710E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3269e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.011          19.208       0.0022116        -0.01223
v  Velocity[Y]              -15.49           15.46         0.27801         0.39418
v  Velocity[Z]             -25.547          12.036         -1.6397        -0.50785
v  ǁVelocityǁ         0.00033817           25.71          7.6661          6.5479
v  Pressure                 -559.1          205.88          29.906          34.882
v  k                   9.8261e-011          7.0425         0.23665         0.51467
v  omega                    57.494     2.7317e+008     1.2912e+006           76862
v  TempK                    298.56          363.17          337.67          346.34
v  TurbVisc            2.4624e-018       0.0019845     6.0071e-005      0.00021191
v  CourantNb             0.0001223          1.5806         0.78966         0.97043
v  FourierNb             0.0038155               1         0.41872         0.18375
v  total_pressure      1.0077e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0031904     7.4109e-005      0.00020359

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.48          306.57
v  Yplus               0          2.9197         0.62917         0.48446


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47286          2.1754          1.2084          1.1542


 INSTANT    0.822000000E-02   TIME STEP NUMBER             822
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925344E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13773E-01 0.46673E+01
   Friction velocity        uk    :  0.13773E-01 0.46634E+01
   Dimensionless distance   yplus :  0.93383E-02 0.29195E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.18063E+03
   Rough dim-less th. sca.  tplus :  0.66153E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27185E+00      10   0.14431E-04   0.47397E+01 0.35846E+02 
c  Velocity[X]                                      0.21331E+01 
c  Velocity[Y]                                      0.12157E+01 
c  Velocity[Z]                                      0.13910E+01 
c  Pressure     0.16763E-04      18   0.29483E-03   0.17075E-01 0.20370E+02 
c  k            0.19937E-01      12   0.58586E-04   0.12179E+00 0.50738E+02 
c  omega        0.27922E+07       1   0.98192E-07   0.17153E+08 0.71904E+00 
c  TempK        0.10053E+05       4   0.51861E-05   0.51814E+01 0.82699E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3258e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.016           19.21       0.0021465       -0.012305
v  Velocity[Y]              -15.65          15.461         0.27845           0.395
v  Velocity[Z]             -25.544          12.036         -1.6396        -0.50788
v  ǁVelocityǁ         0.00033628          25.707          7.6657          6.5472
v  Pressure                -559.31          205.77          29.798           34.78
v  k                   9.8253e-011           7.061         0.23684         0.51517
v  omega                    57.495     2.7317e+008     1.2912e+006           76862
v  TempK                    298.56          363.17          337.67          346.35
v  TurbVisc            2.4623e-018       0.0019963     6.0131e-005      0.00021214
v  CourantNb            0.00012494          1.5808         0.78964         0.97041
v  FourierNb             0.0038155               1         0.41877         0.18391
v  total_pressure      1.0077e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0033254     7.4111e-005       0.0002036

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.48          306.57
v  Yplus               0          2.9195         0.62915         0.48444


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44236          2.1757          1.2084          1.1543


 INSTANT    0.823000000E-02   TIME STEP NUMBER             823
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925296E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13480E-01 0.46673E+01
   Friction velocity        uk    :  0.13480E-01 0.46634E+01
   Dimensionless distance   yplus :  0.91399E-02 0.29193E+01
   Friction thermal sca.    tstar :  0.12148E+01 0.18455E+03
   Rough dim-less th. sca.  tplus :  0.64748E-02 0.20681E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27181E+00      10   0.14733E-04   0.47544E+01 0.35930E+02 
c  Velocity[X]                                      0.21424E+01 
c  Velocity[Y]                                      0.12212E+01 
c  Velocity[Z]                                      0.13908E+01 
c  Pressure     0.16713E-04      18   0.28893E-03   0.17030E-01 0.20750E+02 
c  k            0.19954E-01      12   0.59686E-04   0.12285E+00 0.50877E+02 
c  omega        0.27922E+07       1   0.95376E-07   0.12791E+08 0.64558E+00 
c  TempK        0.10053E+05       4   0.51742E-05   0.51704E+01 0.82657E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3253e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.02          19.212       0.0020818       -0.012376
v  Velocity[Y]             -15.607          15.461         0.27889         0.39582
v  Velocity[Z]             -25.541          12.036         -1.6395        -0.50791
v  ǁVelocityǁ         0.00033447          25.704          7.6654          6.5465
v  Pressure                -559.51          205.65          29.687          34.676
v  k                   9.8246e-011          7.1799         0.23703         0.51566
v  omega                    57.495     2.7317e+008     1.2912e+006           76861
v  TempK                    298.56          363.17          337.68          346.36
v  TurbVisc            2.4621e-018       0.0020083     6.0191e-005      0.00021236
v  CourantNb            0.00012744           1.581         0.78961         0.97039
v  FourierNb             0.0038155               1         0.41883         0.18406
v  total_pressure      1.0077e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035629     7.4115e-005      0.00020361

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.48          306.57
v  Yplus               0          2.9193         0.62914         0.48441


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43241          2.1759          1.2084          1.1545


 INSTANT    0.824000000E-02   TIME STEP NUMBER             824
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925297E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13184E-01 0.46673E+01
   Friction velocity        uk    :  0.13184E-01 0.46634E+01
   Dimensionless distance   yplus :  0.89388E-02 0.29192E+01
   Friction thermal sca.    tstar :  0.12148E+01 0.18870E+03
   Rough dim-less th. sca.  tplus :  0.63323E-02 0.20680E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27177E+00      10   0.14984E-04   0.47646E+01 0.35954E+02 
c  Velocity[X]                                      0.21519E+01 
c  Velocity[Y]                                      0.12181E+01 
c  Velocity[Z]                                      0.13946E+01 
c  Pressure     0.16516E-04      18   0.29501E-03   0.16835E-01 0.21675E+02 
c  k            0.19971E-01      12   0.60850E-04   0.12414E+00 0.51039E+02 
c  omega        0.27922E+07       1   0.95050E-07   0.12892E+08 0.63949E+00 
c  TempK        0.10052E+05       4   0.51628E-05   0.51658E+01 0.82655E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3252e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.024          19.214        0.002016       -0.012443
v  Velocity[Y]             -15.529          15.461         0.27932         0.39665
v  Velocity[Z]             -25.538          12.036         -1.6394        -0.50794
v  ǁVelocityǁ         0.00033295          25.701           7.665          6.5458
v  Pressure                -559.72          205.53           29.57          34.565
v  k                   9.8239e-011          7.3011         0.23722         0.51615
v  omega                    57.495     2.7317e+008     1.2912e+006           76861
v  TempK                    298.56          363.17          337.69          346.37
v  TurbVisc            2.4619e-018       0.0020205     6.0251e-005      0.00021258
v  CourantNb            0.00012981           1.581         0.78959         0.97038
v  FourierNb             0.0038154               1         0.41889         0.18421
v  total_pressure      1.0077e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0037244     7.4118e-005      0.00020363

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.48          306.57
v  Yplus               0          2.9192         0.62912         0.48438


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39396          2.1759          1.2085          1.1546


 INSTANT    0.825000000E-02   TIME STEP NUMBER             825
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925234E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12912E-01 0.46673E+01
   Friction velocity        uk    :  0.12912E-01 0.46634E+01
   Dimensionless distance   yplus :  0.87543E-02 0.29190E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.19268E+03
   Rough dim-less th. sca.  tplus :  0.62016E-02 0.20678E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27174E+00      10   0.14991E-04   0.47820E+01 0.36028E+02 
c  Velocity[X]                                      0.21621E+01 
c  Velocity[Y]                                      0.12214E+01 
c  Velocity[Z]                                      0.13985E+01 
c  Pressure     0.16726E-04      18   0.31320E-03   0.17054E-01 0.21480E+02 
c  k            0.19987E-01      12   0.62445E-04   0.12569E+00 0.51224E+02 
c  omega        0.27922E+07       1   0.94226E-07   0.11275E+08 0.60613E+00 
c  TempK        0.10052E+05       4   0.51519E-05   0.51618E+01 0.82658E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.325e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.028          19.216       0.0019509       -0.012508
v  Velocity[Y]             -15.485          15.461         0.27975         0.39748
v  Velocity[Z]             -25.535          12.035         -1.6393        -0.50797
v  ǁVelocityǁ         0.00030932          25.698          7.6647          6.5451
v  Pressure                -559.92          205.41          29.454          34.456
v  k                   9.8231e-011          7.4238         0.23741         0.51663
v  omega                    57.495     2.7317e+008     1.2912e+006           76861
v  TempK                    298.56          363.17          337.69          346.38
v  TurbVisc            2.4617e-018       0.0020166     6.0309e-005      0.00021281
v  CourantNb            0.00013198           1.581         0.78956         0.97036
v  FourierNb             0.0038154               1         0.41894         0.18436
v  total_pressure      1.0077e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0033828     7.4122e-005      0.00020364

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.48          306.57
v  Yplus               0           2.919          0.6291         0.48435


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52115          2.1759          1.2085          1.1547


 INSTANT    0.826000000E-02   TIME STEP NUMBER             826
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925310E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12648E-01 0.46674E+01
   Friction velocity        uk    :  0.12648E-01 0.46635E+01
   Dimensionless distance   yplus :  0.85756E-02 0.29188E+01
   Friction thermal sca.    tstar :  0.12145E+01 0.19670E+03
   Rough dim-less th. sca.  tplus :  0.60750E-02 0.20677E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27170E+00      10   0.14929E-04   0.47947E+01 0.36085E+02 
c  Velocity[X]                                      0.21700E+01 
c  Velocity[Y]                                      0.12227E+01 
c  Velocity[Z]                                      0.14020E+01 
c  Pressure     0.16689E-04      18   0.30311E-03   0.17023E-01 0.23041E+02 
c  k            0.20002E-01      12   0.63763E-04   0.12723E+00 0.51421E+02 
c  omega        0.27922E+07       1   0.93516E-07   0.10179E+08 0.58349E+00 
c  TempK        0.10051E+05       4   0.51409E-05   0.51535E+01 0.82650E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3245e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.033          19.218       0.0018866       -0.012566
v  Velocity[Y]             -15.485          15.462         0.28018         0.39831
v  Velocity[Z]             -25.531          12.035         -1.6392          -0.508
v  ǁVelocityǁ         0.00033055          25.695          7.6643          6.5444
v  Pressure                -560.12          205.28          29.328          34.336
v  k                   9.8224e-011          7.5474          0.2376          0.5171
v  omega                    57.495     2.7317e+008     1.2912e+006           76861
v  TempK                    298.56          363.17           337.7           346.4
v  TurbVisc            2.4615e-018       0.0020116     6.0368e-005      0.00021302
v  CourantNb            0.00013405          1.5811         0.78954         0.97034
v  FourierNb             0.0038153               1           0.419         0.18451
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0033688     7.4126e-005      0.00020365

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.48          306.57
v  Yplus               0          2.9188         0.62908         0.48432


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65832          2.1761          1.2085          1.1548


 INSTANT    0.827000000E-02   TIME STEP NUMBER             827
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925329E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12446E-01 0.46674E+01
   Friction velocity        uk    :  0.12446E-01 0.46635E+01
   Dimensionless distance   yplus :  0.84386E-02 0.29186E+01
   Friction thermal sca.    tstar :  0.12145E+01 0.19989E+03
   Rough dim-less th. sca.  tplus :  0.59779E-02 0.20675E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27166E+00      10   0.14926E-04   0.48052E+01 0.36123E+02 
c  Velocity[X]                                      0.21744E+01 
c  Velocity[Y]                                      0.12234E+01 
c  Velocity[Z]                                      0.14074E+01 
c  Pressure     0.16725E-04      18   0.30012E-03   0.17065E-01 0.23970E+02 
c  k            0.20018E-01      12   0.65082E-04   0.12881E+00 0.51641E+02 
c  omega        0.27922E+07       1   0.95127E-07   0.14040E+08 0.64990E+00 
c  TempK        0.10051E+05       4   0.51301E-05   0.51450E+01 0.82640E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3237e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.037           19.22        0.001824       -0.012621
v  Velocity[Y]             -15.569          15.462          0.2806         0.39915
v  Velocity[Z]             -25.528          12.033         -1.6391        -0.50802
v  ǁVelocityǁ         0.00032948          25.691          7.6639          6.5437
v  Pressure                -560.31          205.14          29.195          34.209
v  k                   9.8216e-011          7.6712         0.23778         0.51757
v  omega                    57.495     2.7317e+008     1.2912e+006           76860
v  TempK                    298.56          363.17           337.7          346.41
v  TurbVisc            2.4613e-018       0.0020117     6.0427e-005      0.00021324
v  CourantNb            0.00013587          1.5814         0.78952         0.97033
v  FourierNb             0.0038153               1         0.41905         0.18465
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.003346     7.4129e-005      0.00020367

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.48          306.57
v  Yplus               0          2.9186         0.62906          0.4843


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58321          2.1763          1.2086           1.155


 INSTANT    0.828000000E-02   TIME STEP NUMBER             828
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925234E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12220E-01 0.46674E+01
   Friction velocity        uk    :  0.12220E-01 0.46635E+01
   Dimensionless distance   yplus :  0.82855E-02 0.29184E+01
   Friction thermal sca.    tstar :  0.12148E+01 0.20359E+03
   Rough dim-less th. sca.  tplus :  0.58695E-02 0.20674E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27162E+00      10   0.14787E-04   0.48185E+01 0.36170E+02 
c  Velocity[X]                                      0.21796E+01 
c  Velocity[Y]                                      0.12264E+01 
c  Velocity[Z]                                      0.14126E+01 
c  Pressure     0.16828E-04      18   0.29892E-03   0.17175E-01 0.23583E+02 
c  k            0.20033E-01      12   0.66380E-04   0.13039E+00 0.51876E+02 
c  omega        0.27922E+07       1   0.96618E-07   0.19974E+08 0.74232E+00 
c  TempK        0.10050E+05       4   0.51195E-05   0.51370E+01 0.82652E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3228e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.041          19.222       0.0017611       -0.012674
v  Velocity[Y]             -15.616          15.462         0.28101         0.39998
v  Velocity[Z]             -25.524          12.032          -1.639        -0.50805
v  ǁVelocityǁ         0.00031872          25.688          7.6636          6.5431
v  Pressure                -560.49             205          29.065          34.086
v  k                   9.8209e-011          7.7946         0.23797         0.51803
v  omega                    57.495     2.7317e+008     1.2912e+006           76860
v  TempK                    298.56          363.17          337.71          346.42
v  TurbVisc            2.4612e-018       0.0020171     6.0486e-005      0.00021345
v  CourantNb            0.00013752          1.5816          0.7895         0.97031
v  FourierNb             0.0038152               1         0.41911         0.18479
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0033054     7.4132e-005      0.00020368

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.48          306.57
v  Yplus               0          2.9184         0.62904         0.48427


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63014          2.1765          1.2086          1.1551


 INSTANT    0.829000000E-02   TIME STEP NUMBER             829
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925339E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12052E-01 0.46674E+01
   Friction velocity        uk    :  0.12052E-01 0.46635E+01
   Dimensionless distance   yplus :  0.81717E-02 0.29182E+01
   Friction thermal sca.    tstar :  0.12150E+01 0.20642E+03
   Rough dim-less th. sca.  tplus :  0.57889E-02 0.20673E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27158E+00      10   0.14540E-04   0.48317E+01 0.36218E+02 
c  Velocity[X]                                      0.21844E+01 
c  Velocity[Y]                                      0.12304E+01 
c  Velocity[Z]                                      0.14169E+01 
c  Pressure     0.16825E-04      18   0.30072E-03   0.17178E-01 0.24560E+02 
c  k            0.20048E-01      12   0.67550E-04   0.13186E+00 0.52105E+02 
c  omega        0.27922E+07       1   0.94890E-07   0.15339E+08 0.67173E+00 
c  TempK        0.10050E+05       4   0.51088E-05   0.51303E+01 0.82649E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3227e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.045          19.224       0.0016962       -0.012725
v  Velocity[Y]             -15.539          15.461         0.28142         0.40082
v  Velocity[Z]             -25.521           12.03         -1.6389        -0.50807
v  ǁVelocityǁ         0.00030634          25.685          7.6632          6.5424
v  Pressure                -560.67          204.86          28.928          33.956
v  k                   9.8201e-011          7.9167         0.23815         0.51848
v  omega                    57.495     2.7317e+008     1.2912e+006           76860
v  TempK                    298.56          363.17          337.72          346.43
v  TurbVisc             2.461e-018       0.0020225     6.0544e-005      0.00021367
v  CourantNb            0.00013902          1.5816         0.78948          0.9703
v  FourierNb             0.0038152               1         0.41916         0.18493
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0032984     7.4134e-005      0.00020369

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.48          306.57
v  Yplus               0          2.9182         0.62902         0.48425


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60954          2.1765          1.2086          1.1552


 INSTANT    0.830000000E-02   TIME STEP NUMBER             830
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925303E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11900E-01 0.46674E+01
   Friction velocity        uk    :  0.11900E-01 0.46635E+01
   Dimensionless distance   yplus :  0.80686E-02 0.29180E+01
   Friction thermal sca.    tstar :  0.12148E+01 0.20906E+03
   Rough dim-less th. sca.  tplus :  0.57158E-02 0.20671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27155E+00      10   0.14552E-04   0.48411E+01 0.36212E+02 
c  Velocity[X]                                      0.21916E+01 
c  Velocity[Y]                                      0.12269E+01 
c  Velocity[Z]                                      0.14227E+01 
c  Pressure     0.17218E-04      18   0.31128E-03   0.17584E-01 0.25250E+02 
c  k            0.20063E-01      12   0.68497E-04   0.13287E+00 0.52297E+02 
c  omega        0.27922E+07       1   0.92201E-07   0.79824E+07 0.53393E+00 
c  TempK        0.10049E+05       4   0.50988E-05   0.51311E+01 0.82683E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3228e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.05          19.226       0.0016335       -0.012773
v  Velocity[Y]             -15.479          15.461         0.28182         0.40165
v  Velocity[Z]             -25.517          12.029         -1.6389        -0.50809
v  ǁVelocityǁ         0.00029458          25.681          7.6628          6.5418
v  Pressure                -560.85          204.71          28.787          33.821
v  k                   9.8194e-011          8.0369         0.23833         0.51893
v  omega                    57.495     2.7317e+008     1.2912e+006           76859
v  TempK                    298.56          363.17          337.72          346.44
v  TurbVisc            2.4608e-018       0.0020278     6.0602e-005      0.00021388
v  CourantNb            0.00014037          1.5816         0.78945         0.97028
v  FourierNb             0.0038152               1         0.41922         0.18507
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0033307     7.4137e-005      0.00020369

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.48          306.57
v  Yplus               0           2.918           0.629         0.48422


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53038          2.1765          1.2087          1.1553


 INSTANT    0.831000000E-02   TIME STEP NUMBER             831
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925198E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11790E-01 0.46674E+01
   Friction velocity        uk    :  0.11790E-01 0.46635E+01
   Dimensionless distance   yplus :  0.79937E-02 0.29178E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.21102E+03
   Rough dim-less th. sca.  tplus :  0.56628E-02 0.20670E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27151E+00      10   0.14550E-04   0.48574E+01 0.36254E+02 
c  Velocity[X]                                      0.21992E+01 
c  Velocity[Y]                                      0.12288E+01 
c  Velocity[Z]                                      0.14294E+01 
c  Pressure     0.17541E-04      19   0.32005E-03   0.17918E-01 0.24995E+02 
c  k            0.20077E-01      12   0.69590E-04   0.13389E+00 0.52473E+02 
c  omega        0.27922E+07       1   0.91931E-07   0.76659E+07 0.52622E+00 
c  TempK        0.10049E+05       4   0.50890E-05   0.51352E+01 0.82724E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3225e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.054          19.227        0.001572        -0.01282
v  Velocity[Y]             -15.469          15.461         0.28221         0.40249
v  Velocity[Z]             -25.514          12.027         -1.6388        -0.50811
v  ǁVelocityǁ         0.00028295          25.678          7.6624          6.5412
v  Pressure                -561.01          204.55          28.647          33.688
v  k                   9.8186e-011          8.1543          0.2385         0.51938
v  omega                    57.495     2.7317e+008     1.2912e+006           76859
v  TempK                    298.57          363.17          337.73          346.45
v  TurbVisc            2.4606e-018       0.0020331     6.0659e-005      0.00021409
v  CourantNb            0.00014154          1.5817         0.78942         0.97026
v  FourierNb             0.0038151               1         0.41927          0.1852
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0033408     7.4139e-005       0.0002037

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.48          306.57
v  Yplus               0          2.9178         0.62898         0.48419


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40568          2.1766          1.2087          1.1555


 INSTANT    0.832000000E-02   TIME STEP NUMBER             832
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925233E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11695E-01 0.46675E+01
   Friction velocity        uk    :  0.11695E-01 0.46635E+01
   Dimensionless distance   yplus :  0.79291E-02 0.29177E+01
   Friction thermal sca.    tstar :  0.12145E+01 0.21274E+03
   Rough dim-less th. sca.  tplus :  0.56170E-02 0.20669E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27148E+00      10   0.14502E-04   0.48782E+01 0.36322E+02 
c  Velocity[X]                                      0.22077E+01 
c  Velocity[Y]                                      0.12318E+01 
c  Velocity[Z]                                      0.14386E+01 
c  Pressure     0.17731E-04      19   0.31386E-03   0.18117E-01 0.25055E+02 
c  k            0.20091E-01      12   0.70633E-04   0.13490E+00 0.52637E+02 
c  omega        0.27922E+07       1   0.94436E-07   0.13191E+08 0.62575E+00 
c  TempK        0.10049E+05       4   0.50795E-05   0.51370E+01 0.82759E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3219e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.058          19.229       0.0015082       -0.012868
v  Velocity[Y]             -15.546          15.461         0.28261         0.40333
v  Velocity[Z]              -25.51          12.024         -1.6387        -0.50813
v  ǁVelocityǁ          0.0002718          25.675          7.6621          6.5406
v  Pressure                -561.16          204.41          28.508          33.555
v  k                   9.8178e-011          8.2683         0.23868         0.51982
v  omega                    57.495     2.7317e+008     1.2912e+006           76859
v  TempK                    298.57          363.17          337.73          346.46
v  TurbVisc            2.4604e-018       0.0020381     6.0716e-005       0.0002143
v  CourantNb            0.00014252          1.5818          0.7894         0.97024
v  FourierNb             0.0038151               1         0.41932         0.18533
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0033405     7.4142e-005      0.00020371

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.48          306.57
v  Yplus               0          2.9177         0.62896         0.48416


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54074          2.1767          1.2087          1.1556


 INSTANT    0.833000000E-02   TIME STEP NUMBER             833
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925221E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11651E-01 0.46675E+01
   Friction velocity        uk    :  0.11651E-01 0.46636E+01
   Dimensionless distance   yplus :  0.78996E-02 0.29175E+01
   Friction thermal sca.    tstar :  0.12148E+01 0.21354E+03
   Rough dim-less th. sca.  tplus :  0.55961E-02 0.20667E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27144E+00      10   0.14537E-04   0.49010E+01 0.36413E+02 
c  Velocity[X]                                      0.22160E+01 
c  Velocity[Y]                                      0.12390E+01 
c  Velocity[Z]                                      0.14459E+01 
c  Pressure     0.17923E-04      19   0.31553E-03   0.18316E-01 0.25345E+02 
c  k            0.20105E-01      12   0.71775E-04   0.13600E+00 0.52807E+02 
c  omega        0.27922E+07       1   0.97687E-07   0.24488E+08 0.80122E+00 
c  TempK        0.10048E+05       4   0.50699E-05   0.51340E+01 0.82772E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3213e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.062          19.231       0.0014467       -0.012916
v  Velocity[Y]             -15.596           15.46         0.28299         0.40417
v  Velocity[Z]             -25.507          12.022         -1.6386        -0.50815
v  ǁVelocityǁ         0.00026062          25.671          7.6617          6.5399
v  Pressure                -561.29          204.25          28.367           33.42
v  k                    9.817e-011          8.3783         0.23885         0.52025
v  omega                    57.496     2.7317e+008     1.2912e+006           76859
v  TempK                    298.57          363.17          337.74          346.47
v  TurbVisc            2.4602e-018       0.0020429     6.0773e-005       0.0002145
v  CourantNb            0.00014331           1.582         0.78937         0.97022
v  FourierNb              0.003815               1         0.41937         0.18546
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0032623     7.4147e-005      0.00020371

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.49          306.57
v  Yplus               0          2.9175         0.62894         0.48413


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46501          2.1769          1.2087          1.1557


 INSTANT    0.834000000E-02   TIME STEP NUMBER             834
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925241E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11632E-01 0.46675E+01
   Friction velocity        uk    :  0.11632E-01 0.46636E+01
   Dimensionless distance   yplus :  0.78869E-02 0.29172E+01
   Friction thermal sca.    tstar :  0.12151E+01 0.21388E+03
   Rough dim-less th. sca.  tplus :  0.55871E-02 0.20666E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27140E+00      10   0.14599E-04   0.49121E+01 0.36440E+02 
c  Velocity[X]                                      0.22196E+01 
c  Velocity[Y]                                      0.12414E+01 
c  Velocity[Z]                                      0.14511E+01 
c  Pressure     0.17932E-04      18   0.31770E-03   0.18327E-01 0.26994E+02 
c  k            0.20119E-01      12   0.72980E-04   0.13708E+00 0.52991E+02 
c  omega        0.27922E+07       1   0.95095E-07   0.16945E+08 0.69005E+00 
c  TempK        0.10048E+05       4   0.50602E-05   0.51330E+01 0.82741E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3214e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.067          19.232       0.0013827       -0.012961
v  Velocity[Y]             -15.533          15.459         0.28338         0.40501
v  Velocity[Z]             -25.503          12.019         -1.6386        -0.50818
v  ǁVelocityǁ         0.00024979          25.667          7.6613          6.5393
v  Pressure                -561.42          204.09          28.215          33.274
v  k                   9.8162e-011          8.4833         0.23903         0.52069
v  omega                    57.496     2.7317e+008     1.2912e+006           76858
v  TempK                    298.57          363.17          337.75          346.48
v  TurbVisc              2.46e-018       0.0020476     6.0829e-005      0.00021471
v  CourantNb            0.00014396          1.5819         0.78935          0.9702
v  FourierNb              0.003815               1         0.41942         0.18558
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0032178      7.415e-005      0.00020372

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.49          306.58
v  Yplus               0          2.9172         0.62892          0.4841


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.28121          2.1769          1.2088          1.1558


 INSTANT    0.835000000E-02   TIME STEP NUMBER             835
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925344E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11658E-01 0.46675E+01
   Friction velocity        uk    :  0.11658E-01 0.46636E+01
   Dimensionless distance   yplus :  0.79041E-02 0.29170E+01
   Friction thermal sca.    tstar :  0.12149E+01 0.21342E+03
   Rough dim-less th. sca.  tplus :  0.55993E-02 0.20664E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27137E+00      10   0.14647E-04   0.49161E+01 0.36403E+02 
c  Velocity[X]                                      0.22235E+01 
c  Velocity[Y]                                      0.12364E+01 
c  Velocity[Z]                                      0.14562E+01 
c  Pressure     0.18038E-04      19   0.31560E-03   0.18438E-01 0.28081E+02 
c  k            0.20132E-01      12   0.74317E-04   0.13834E+00 0.53194E+02 
c  omega        0.27922E+07       1   0.91650E-07   0.78506E+07 0.51919E+00 
c  TempK        0.10048E+05       4   0.50505E-05   0.51271E+01 0.82715E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3217e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.071          19.234        0.001321       -0.013005
v  Velocity[Y]             -15.472          15.459         0.28376         0.40585
v  Velocity[Z]             -25.499          12.017         -1.6385         -0.5082
v  ǁVelocityǁ         0.00023917          25.663          7.6609          6.5387
v  Pressure                -561.56          203.92          28.055          33.121
v  k                   9.8155e-011          8.5829          0.2392         0.52112
v  omega                    57.496     2.7317e+008     1.2912e+006           76858
v  TempK                    298.58          363.17          337.75          346.49
v  TurbVisc            2.4598e-018        0.002052     6.0885e-005      0.00021491
v  CourantNb            0.00014439          1.5819         0.78933         0.97019
v  FourierNb             0.0038149               1         0.41947         0.18571
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0031611     7.4154e-005      0.00020372

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.49          306.58
v  Yplus               0           2.917         0.62889         0.48407


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.32229          2.1768          1.2088          1.1559


 INSTANT    0.836000000E-02   TIME STEP NUMBER             836
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925224E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11726E-01 0.46675E+01
   Friction velocity        uk    :  0.11726E-01 0.46636E+01
   Dimensionless distance   yplus :  0.79505E-02 0.29168E+01
   Friction thermal sca.    tstar :  0.12145E+01 0.21217E+03
   Rough dim-less th. sca.  tplus :  0.56322E-02 0.20663E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27134E+00      10   0.14626E-04   0.49271E+01 0.36418E+02 
c  Velocity[X]                                      0.22273E+01 
c  Velocity[Y]                                      0.12373E+01 
c  Velocity[Z]                                      0.14625E+01 
c  Pressure     0.17932E-04      18   0.31775E-03   0.18332E-01 0.27864E+02 
c  k            0.20146E-01      12   0.75591E-04   0.13967E+00 0.53414E+02 
c  omega        0.27922E+07       1   0.91475E-07   0.73030E+07 0.50879E+00 
c  TempK        0.10047E+05       4   0.50409E-05   0.51186E+01 0.82680E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3217e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.075          19.235       0.0012616       -0.013048
v  Velocity[Y]              -15.46          15.458         0.28414          0.4067
v  Velocity[Z]             -25.495          12.014         -1.6384        -0.50822
v  ǁVelocityǁ         0.00022907          25.659          7.6605          6.5382
v  Pressure                -561.68          203.75          27.897          32.969
v  k                   9.8146e-011          8.6766         0.23937         0.52155
v  omega                    57.496     2.7317e+008     1.2912e+006           76858
v  TempK                    298.58          363.17          337.76           346.5
v  TurbVisc            2.4596e-018        0.002056      6.094e-005      0.00021512
v  CourantNb            0.00014469          1.5819          0.7893         0.97017
v  FourierNb             0.0038149               1         0.41953         0.18583
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0032257     7.4157e-005      0.00020373

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.49          306.58
v  Yplus               0          2.9168         0.62887         0.48404


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5637          2.1768          1.2088           1.156


 INSTANT    0.837000000E-02   TIME STEP NUMBER             837
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925317E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11822E-01 0.46675E+01
   Friction velocity        uk    :  0.11822E-01 0.46636E+01
   Dimensionless distance   yplus :  0.80156E-02 0.29166E+01
   Friction thermal sca.    tstar :  0.12146E+01 0.21045E+03
   Rough dim-less th. sca.  tplus :  0.56783E-02 0.20661E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27130E+00      10   0.14593E-04   0.49370E+01 0.36438E+02 
c  Velocity[X]                                      0.22290E+01 
c  Velocity[Y]                                      0.12380E+01 
c  Velocity[Z]                                      0.14700E+01 
c  Pressure     0.17526E-04      19   0.31915E-03   0.17919E-01 0.28150E+02 
c  k            0.20159E-01      12   0.76754E-04   0.14117E+00 0.53658E+02 
c  omega        0.27922E+07       1   0.92632E-07   0.98011E+07 0.55788E+00 
c  TempK        0.10047E+05       4   0.50313E-05   0.51085E+01 0.82642E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3214e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.079          19.236       0.0012034        -0.01309
v  Velocity[Y]             -15.535          15.457         0.28452         0.40754
v  Velocity[Z]             -25.491          12.011         -1.6383        -0.50823
v  ǁVelocityǁ         0.00021934          25.656          7.6601          6.5376
v  Pressure                -561.79          203.57          27.737          32.815
v  k                   9.8138e-011          8.7642         0.23954         0.52197
v  omega                    57.496     2.7317e+008     1.2912e+006           76858
v  TempK                    298.59          363.17          337.76          346.51
v  TurbVisc            2.4594e-018       0.0020596     6.0995e-005      0.00021532
v  CourantNb             0.0001448          1.5819         0.78928         0.97015
v  FourierNb             0.0038148               1         0.41958         0.18595
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0032534     7.4159e-005      0.00020373

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.49          306.58
v  Yplus               0          2.9166         0.62885         0.48402


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62033          2.1769          1.2089          1.1561


 INSTANT    0.838000000E-02   TIME STEP NUMBER             838
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925381E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11962E-01 0.46676E+01
   Friction velocity        uk    :  0.11962E-01 0.46636E+01
   Dimensionless distance   yplus :  0.81102E-02 0.29164E+01
   Friction thermal sca.    tstar :  0.12149E+01 0.20800E+03
   Rough dim-less th. sca.  tplus :  0.57453E-02 0.20660E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27127E+00      10   0.14568E-04   0.49488E+01 0.36471E+02 
c  Velocity[X]                                      0.22309E+01 
c  Velocity[Y]                                      0.12411E+01 
c  Velocity[Z]                                      0.14769E+01 
c  Pressure     0.17484E-04      18   0.32058E-03   0.17877E-01 0.29367E+02 
c  k            0.20171E-01      12   0.78071E-04   0.14280E+00 0.53914E+02 
c  omega        0.27922E+07       1   0.94527E-07   0.15050E+08 0.65179E+00 
c  TempK        0.10047E+05       4   0.50218E-05   0.51019E+01 0.82626E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.321e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.083          19.238       0.0011477       -0.013134
v  Velocity[Y]             -15.587          15.456         0.28489         0.40839
v  Velocity[Z]             -25.487          12.008         -1.6383        -0.50825
v  ǁVelocityǁ         0.00021026          25.652          7.6597           6.537
v  Pressure                 -561.9          203.39           27.57          32.654
v  k                    9.813e-011          8.8456         0.23971         0.52239
v  omega                    57.496     2.7317e+008     1.2912e+006           76857
v  TempK                    298.59          363.17          337.77          346.52
v  TurbVisc            2.4592e-018       0.0020626      6.105e-005      0.00021552
v  CourantNb             0.0001448           1.582         0.78926         0.97013
v  FourierNb             0.0038148               1         0.41963         0.18607
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0032408     7.4161e-005      0.00020373

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.49          306.58
v  Yplus               0          2.9164         0.62883         0.48399


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62334           2.177          1.2089          1.1562


 INSTANT    0.839000000E-02   TIME STEP NUMBER             839
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925234E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12117E-01 0.46676E+01
   Friction velocity        uk    :  0.12117E-01 0.46637E+01
   Dimensionless distance   yplus :  0.82158E-02 0.29162E+01
   Friction thermal sca.    tstar :  0.12152E+01 0.20532E+03
   Rough dim-less th. sca.  tplus :  0.58201E-02 0.20659E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27124E+00      10   0.14620E-04   0.49589E+01 0.36507E+02 
c  Velocity[X]                                      0.22289E+01 
c  Velocity[Y]                                      0.12452E+01 
c  Velocity[Z]                                      0.14849E+01 
c  Pressure     0.17179E-04      18   0.32444E-03   0.17566E-01 0.28335E+02 
c  k            0.20184E-01      12   0.79383E-04   0.14447E+00 0.54171E+02 
c  omega        0.27922E+07       1   0.95374E-07   0.17289E+08 0.68948E+00 
c  TempK        0.10047E+05       4   0.50126E-05   0.50961E+01 0.82602E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3214e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.087          19.239       0.0010916       -0.013179
v  Velocity[Y]             -15.524          15.455         0.28527         0.40923
v  Velocity[Z]             -25.483          12.005         -1.6382        -0.50826
v  ǁVelocityǁ         0.00020184          25.648          7.6593          6.5364
v  Pressure                   -562          203.22           27.41            32.5
v  k                   9.8122e-011          8.9209         0.23987         0.52281
v  omega                    57.496     2.7317e+008     1.2912e+006           76857
v  TempK                    298.58          363.17          337.78          346.53
v  TurbVisc             2.459e-018        0.002065     6.1105e-005      0.00021572
v  CourantNb            0.00014035          1.5819         0.78923         0.97012
v  FourierNb             0.0038147               1         0.41968         0.18619
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0032026     7.4164e-005      0.00020373

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.49          306.58
v  Yplus               0          2.9162         0.62881         0.48396


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49331          2.1769          1.2089          1.1563


 INSTANT    0.840000000E-02   TIME STEP NUMBER             840
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925336E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12308E-01 0.46676E+01
   Friction velocity        uk    :  0.12308E-01 0.46637E+01
   Dimensionless distance   yplus :  0.83447E-02 0.29161E+01
   Friction thermal sca.    tstar :  0.12150E+01 0.20215E+03
   Rough dim-less th. sca.  tplus :  0.59114E-02 0.20658E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27120E+00      10   0.14767E-04   0.49625E+01 0.36493E+02 
c  Velocity[X]                                      0.22267E+01 
c  Velocity[Y]                                      0.12449E+01 
c  Velocity[Z]                                      0.14909E+01 
c  Pressure     0.17298E-04      19   0.32186E-03   0.17690E-01 0.30634E+02 
c  k            0.20196E-01      12   0.80723E-04   0.14613E+00 0.54422E+02 
c  omega        0.27922E+07       1   0.93524E-07   0.13370E+08 0.62226E+00 
c  TempK        0.10046E+05       4   0.50036E-05   0.50900E+01 0.82580E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.322e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.091           19.24       0.0010414       -0.013223
v  Velocity[Y]             -15.462          15.453         0.28565         0.41008
v  Velocity[Z]             -25.478          12.002         -1.6382        -0.50827
v  ǁVelocityǁ         0.00019445          25.644          7.6589          6.5359
v  Pressure                -562.12          203.03          27.235          32.331
v  k                   9.8114e-011          8.9902         0.24004         0.52322
v  omega                    57.496     2.7317e+008     1.2912e+006           76857
v  TempK                    298.58          363.17          337.78          346.54
v  TurbVisc            2.4588e-018       0.0020667      6.116e-005      0.00021592
v  CourantNb            0.00011819          1.5818         0.78921          0.9701
v  FourierNb             0.0038147               1         0.41973         0.18631
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006         0.00315     7.4167e-005      0.00020373

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.49          306.58
v  Yplus               0          2.9161         0.62879         0.48393


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41859          2.1767          1.2089          1.1564


 INSTANT    0.841000000E-02   TIME STEP NUMBER             841
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925196E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12490E-01 0.46676E+01
   Friction velocity        uk    :  0.12490E-01 0.46637E+01
   Dimensionless distance   yplus :  0.84686E-02 0.29165E+01
   Friction thermal sca.    tstar :  0.12147E+01 0.19919E+03
   Rough dim-less th. sca.  tplus :  0.59992E-02 0.20661E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27117E+00      10   0.14734E-04   0.49666E+01 0.36473E+02 
c  Velocity[X]                                      0.22238E+01 
c  Velocity[Y]                                      0.12453E+01 
c  Velocity[Z]                                      0.14975E+01 
c  Pressure     0.16856E-04      18   0.31904E-03   0.17239E-01 0.31192E+02 
c  k            0.20208E-01      12   0.81970E-04   0.14783E+00 0.54679E+02 
c  omega        0.27922E+07       1   0.92113E-07   0.90209E+07 0.54277E+00 
c  TempK        0.10046E+05       4   0.49944E-05   0.50817E+01 0.82539E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3223e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.095          19.241      0.00099417       -0.013265
v  Velocity[Y]              -15.45          15.452         0.28602         0.41092
v  Velocity[Z]             -25.474          11.999         -1.6381        -0.50828
v  ǁVelocityǁ         0.00018781          25.639          7.6585          6.5353
v  Pressure                -562.25          202.84          27.057          32.158
v  k                   9.8105e-011          9.0535         0.24021         0.52363
v  omega                    57.496     2.7317e+008     1.2912e+006           76857
v  TempK                    298.58          363.17          337.79          346.55
v  TurbVisc            2.4586e-018       0.0020686     6.1214e-005      0.00021611
v  CourantNb            0.00010576          1.5817         0.78919         0.97009
v  FourierNb             0.0038146               1         0.41978         0.18643
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0031819     7.4169e-005      0.00020373

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.49          306.58
v  Yplus               0          2.9165         0.62877          0.4839


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.36152          2.1767           1.209          1.1565


 INSTANT    0.842000000E-02   TIME STEP NUMBER             842
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925370E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12717E-01 0.46676E+01
   Friction velocity        uk    :  0.12717E-01 0.46637E+01
   Dimensionless distance   yplus :  0.86221E-02 0.29169E+01
   Friction thermal sca.    tstar :  0.12148E+01 0.19565E+03
   Rough dim-less th. sca.  tplus :  0.61080E-02 0.20663E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27114E+00      10   0.14768E-04   0.49722E+01 0.36464E+02 
c  Velocity[X]                                      0.22204E+01 
c  Velocity[Y]                                      0.12464E+01 
c  Velocity[Z]                                      0.15054E+01 
c  Pressure     0.16784E-04      18   0.31647E-03   0.17167E-01 0.32700E+02 
c  k            0.20220E-01      12   0.83099E-04   0.14964E+00 0.54941E+02 
c  omega        0.27922E+07       1   0.92501E-07   0.10050E+08 0.56079E+00 
c  TempK        0.10046E+05       4   0.49857E-05   0.50759E+01 0.82509E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3224e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.098          19.242       0.0009502       -0.013305
v  Velocity[Y]             -15.527          15.451          0.2864         0.41176
v  Velocity[Z]             -25.469          11.996          -1.638        -0.50829
v  ǁVelocityǁ         0.00018197          25.635          7.6581          6.5347
v  Pressure                -562.36          202.64          26.869          31.976
v  k                   9.8097e-011          9.1109         0.24037         0.52404
v  omega                    57.496     2.7317e+008     1.2912e+006           76856
v  TempK                    298.58          363.17          337.79          346.56
v  TurbVisc            2.4584e-018       0.0020713     6.1268e-005      0.00021631
v  CourantNb            0.00010253          1.5817         0.78916         0.97007
v  FourierNb             0.0038145               1         0.41983         0.18655
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0032775     7.4172e-005      0.00020373

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.49          306.58
v  Yplus               0          2.9169         0.62875         0.48387


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50465          2.1767           1.209          1.1566


 INSTANT    0.843000000E-02   TIME STEP NUMBER             843
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925382E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12944E-01 0.46677E+01
   Friction velocity        uk    :  0.12944E-01 0.46637E+01
   Dimensionless distance   yplus :  0.87760E-02 0.29173E+01
   Friction thermal sca.    tstar :  0.12151E+01 0.19222E+03
   Rough dim-less th. sca.  tplus :  0.62169E-02 0.20666E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27111E+00      10   0.14786E-04   0.49853E+01 0.36490E+02 
c  Velocity[X]                                      0.22176E+01 
c  Velocity[Y]                                      0.12515E+01 
c  Velocity[Z]                                      0.15162E+01 
c  Pressure     0.17187E-04      18   0.31546E-03   0.17580E-01 0.32411E+02 
c  k            0.20231E-01      12   0.84371E-04   0.15163E+00 0.55217E+02 
c  omega        0.27922E+07       1   0.94375E-07   0.14953E+08 0.65044E+00 
c  TempK        0.10046E+05       4   0.49773E-05   0.50692E+01 0.82481E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3224e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.102          19.243      0.00091229       -0.013342
v  Velocity[Y]              -15.58          15.449         0.28676          0.4126
v  Velocity[Z]             -25.464          11.993          -1.638        -0.50829
v  ǁVelocityǁ         0.00017705           25.63          7.6577          6.5342
v  Pressure                -562.48          202.44          26.683          31.796
v  k                   9.8088e-011          9.1626         0.24054         0.52444
v  omega                    57.496     2.7317e+008     1.2912e+006           76856
v  TempK                    298.58          363.17           337.8          346.57
v  TurbVisc            2.4582e-018       0.0020743     6.1322e-005       0.0002165
v  CourantNb           9.8999e-005          1.5817         0.78914         0.97006
v  FourierNb             0.0038145               1         0.41988         0.18666
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0033276     7.4175e-005      0.00020373

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.49          306.58
v  Yplus               0          2.9173         0.62873         0.48385


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55294          2.1767           1.209          1.1567


 INSTANT    0.844000000E-02   TIME STEP NUMBER             844
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925268E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13180E-01 0.46677E+01
   Friction velocity        uk    :  0.13180E-01 0.46638E+01
   Dimensionless distance   yplus :  0.89361E-02 0.29176E+01
   Friction thermal sca.    tstar :  0.12154E+01 0.18878E+03
   Rough dim-less th. sca.  tplus :  0.63304E-02 0.20669E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27108E+00      10   0.14795E-04   0.49969E+01 0.36508E+02 
c  Velocity[X]                                      0.22145E+01 
c  Velocity[Y]                                      0.12578E+01 
c  Velocity[Z]                                      0.15247E+01 
c  Pressure     0.17127E-04      18   0.31928E-03   0.17518E-01 0.32744E+02 
c  k            0.20242E-01      12   0.85536E-04   0.15373E+00 0.55504E+02 
c  omega        0.27922E+07       1   0.94975E-07   0.16624E+08 0.68306E+00 
c  TempK        0.10045E+05       4   0.49694E-05   0.50626E+01 0.82428E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3231e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.106          19.244      0.00087555       -0.013382
v  Velocity[Y]             -15.517          15.447         0.28713         0.41344
v  Velocity[Z]              -25.46           11.99         -1.6379        -0.50828
v  ǁVelocityǁ         0.00017323          25.626          7.6573          6.5336
v  Pressure                 -562.6          202.24          26.496          31.615
v  k                    9.808e-011          9.2089          0.2407         0.52483
v  omega                    57.496     2.7317e+008     1.2912e+006           76856
v  TempK                    298.58          363.17           337.8          346.58
v  TurbVisc             2.458e-018       0.0020837     6.1376e-005       0.0002167
v  CourantNb            0.00010467          1.5815         0.78912         0.97004
v  FourierNb             0.0038144               1         0.41993         0.18678
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0035375     7.4177e-005      0.00020372

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.49          306.58
v  Yplus               0          2.9176         0.62871         0.48382


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45088          2.1765           1.209          1.1568


 INSTANT    0.845000000E-02   TIME STEP NUMBER             845
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925265E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13389E-01 0.46677E+01
   Friction velocity        uk    :  0.13389E-01 0.46638E+01
   Dimensionless distance   yplus :  0.90781E-02 0.29180E+01
   Friction thermal sca.    tstar :  0.12152E+01 0.18582E+03
   Rough dim-less th. sca.  tplus :  0.64310E-02 0.20671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27105E+00      10   0.14840E-04   0.50026E+01 0.36472E+02 
c  Velocity[X]                                      0.22126E+01 
c  Velocity[Y]                                      0.12578E+01 
c  Velocity[Z]                                      0.15321E+01 
c  Pressure     0.17105E-04      20   0.31857E-03   0.17495E-01 0.33865E+02 
c  k            0.20253E-01      12   0.86605E-04   0.15592E+00 0.55794E+02 
c  omega        0.27922E+07       1   0.91715E-07   0.75206E+07 0.51883E+00 
c  TempK        0.10045E+05       4   0.49619E-05   0.50544E+01 0.82377E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3241e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.109          19.244      0.00084077       -0.013423
v  Velocity[Y]             -15.456          15.445         0.28749         0.41427
v  Velocity[Z]             -25.455          11.986         -1.6378        -0.50827
v  ǁVelocityǁ         0.00017034          25.622          7.6569          6.5331
v  Pressure                -562.73          202.04          26.301          31.427
v  k                   9.8071e-011            9.25         0.24087         0.52522
v  omega                    57.496     2.7317e+008     1.2912e+006           76856
v  TempK                    298.58          363.17          337.81          346.59
v  TurbVisc            2.4577e-018       0.0020952      6.143e-005      0.00021689
v  CourantNb            0.00011093          1.5813          0.7891         0.97003
v  FourierNb             0.0038143               1         0.41998          0.1869
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0038913     7.4178e-005      0.00020372

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.49          306.58
v  Yplus               0           2.918         0.62869         0.48379


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51197          2.1763          1.2091          1.1569


 INSTANT    0.846000000E-02   TIME STEP NUMBER             846
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925178E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13626E-01 0.46677E+01
   Friction velocity        uk    :  0.13626E-01 0.46638E+01
   Dimensionless distance   yplus :  0.92385E-02 0.29184E+01
   Friction thermal sca.    tstar :  0.12149E+01 0.18319E+03
   Rough dim-less th. sca.  tplus :  0.65446E-02 0.20674E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27102E+00      10   0.14838E-04   0.50180E+01 0.36497E+02 
c  Velocity[X]                                      0.22135E+01 
c  Velocity[Y]                                      0.12621E+01 
c  Velocity[Z]                                      0.15423E+01 
c  Pressure     0.17439E-04      18   0.32692E-03   0.17837E-01 0.33297E+02 
c  k            0.20264E-01      12   0.87542E-04   0.15817E+00 0.56074E+02 
c  omega        0.27922E+07       1   0.92799E-07   0.93129E+07 0.56129E+00 
c  TempK        0.10045E+05       4   0.49552E-05   0.50447E+01 0.82330E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3247e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.113          19.244      0.00080414       -0.013463
v  Velocity[Y]             -15.444          15.444         0.28785          0.4151
v  Velocity[Z]             -25.451          11.983         -1.6378        -0.50826
v  ǁVelocityǁ         0.00016841          25.617          7.6565          6.5326
v  Pressure                -562.86          201.84          26.112          31.243
v  k                   9.8062e-011          9.2852         0.24103          0.5256
v  omega                    57.496     2.7317e+008     1.2912e+006           76855
v  TempK                    298.58          363.17          337.81           346.6
v  TurbVisc            2.4575e-018       0.0021051     6.1483e-005      0.00021708
v  CourantNb            0.00011735          1.5811         0.78908         0.97001
v  FourierNb             0.0038142               1         0.42003         0.18702
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0042376     7.4179e-005      0.00020372

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.5          306.58
v  Yplus               0          2.9184         0.62868         0.48377


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54763          2.1761          1.2091           1.157


 INSTANT    0.847000000E-02   TIME STEP NUMBER             847
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925283E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13823E-01 0.46677E+01
   Friction velocity        uk    :  0.13823E-01 0.46638E+01
   Dimensionless distance   yplus :  0.93720E-02 0.29188E+01
   Friction thermal sca.    tstar :  0.12150E+01 0.18516E+03
   Rough dim-less th. sca.  tplus :  0.66392E-02 0.20677E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27099E+00      10   0.15091E-04   0.50354E+01 0.36555E+02 
c  Velocity[X]                                      0.22149E+01 
c  Velocity[Y]                                      0.12684E+01 
c  Velocity[Z]                                      0.15521E+01 
c  Pressure     0.18213E-04      19   0.32401E-03   0.18630E-01 0.34060E+02 
c  k            0.20274E-01      13   0.87711E-04   0.16040E+00 0.56352E+02 
c  omega        0.27922E+07       1   0.94585E-07   0.13339E+08 0.63997E+00 
c  TempK        0.10045E+05       4   0.49487E-05   0.50343E+01 0.82275E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3251e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.116          19.245      0.00076862         -0.0135
v  Velocity[Y]             -15.523          15.442         0.28821         0.41593
v  Velocity[Z]             -25.446           11.98         -1.6377        -0.50826
v  ǁVelocityǁ         0.00016719          25.612          7.6561           6.532
v  Pressure                -562.99          201.64          25.917          31.055
v  k                   9.8053e-011          9.3132         0.24119         0.52598
v  omega                    57.496     2.7317e+008     1.2912e+006           76855
v  TempK                    298.57          363.17          337.82          346.61
v  TurbVisc            2.4573e-018       0.0021134     6.1536e-005      0.00021726
v  CourantNb            0.00012387           1.581         0.78906            0.97
v  FourierNb             0.0038141               1         0.42007         0.18713
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0045364     7.4179e-005      0.00020372

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.5          306.58
v  Yplus               0          2.9188         0.62866         0.48374


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55431           2.176          1.2091          1.1571


 INSTANT    0.848000000E-02   TIME STEP NUMBER             848
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925288E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13786E-01 0.46678E+01
   Friction velocity        uk    :  0.13786E-01 0.46639E+01
   Dimensionless distance   yplus :  0.93473E-02 0.29192E+01
   Friction thermal sca.    tstar :  0.12153E+01 0.18757E+03
   Rough dim-less th. sca.  tplus :  0.66217E-02 0.20680E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27096E+00      10   0.15140E-04   0.50566E+01 0.36596E+02 
c  Velocity[X]                                      0.22188E+01 
c  Velocity[Y]                                      0.12743E+01 
c  Velocity[Z]                                      0.15634E+01 
c  Pressure     0.18091E-04      19   0.32523E-03   0.18506E-01 0.35088E+02 
c  k            0.20284E-01      13   0.88478E-04   0.16252E+00 0.56603E+02 
c  omega        0.27922E+07       1   0.96963E-07   0.18833E+08 0.73404E+00 
c  TempK        0.10045E+05       4   0.49424E-05   0.50233E+01 0.82213E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3255e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.119          19.245       0.0007326        -0.01354
v  Velocity[Y]             -15.577          15.439         0.28857         0.41675
v  Velocity[Z]             -25.441          11.977         -1.6377        -0.50825
v  ǁVelocityǁ         0.00016668          25.607          7.6556          6.5315
v  Pressure                -563.12          201.43          25.717           30.86
v  k                   9.8044e-011          9.3345         0.24135         0.52636
v  omega                    57.496     2.7317e+008     1.2912e+006           76855
v  TempK                    298.57          363.17          337.83          346.62
v  TurbVisc            2.4571e-018       0.0021146     6.1589e-005      0.00021745
v  CourantNb            0.00013114          1.5809         0.78903         0.96998
v  FourierNb             0.0038141               1         0.42012         0.18725
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.004704      7.418e-005      0.00020371

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.5          306.58
v  Yplus               0          2.9192         0.62864         0.48372


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47491           2.176          1.2092          1.1572


 INSTANT    0.849000000E-02   TIME STEP NUMBER             849
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925292E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13665E-01 0.46678E+01
   Friction velocity        uk    :  0.13665E-01 0.46639E+01
   Dimensionless distance   yplus :  0.92650E-02 0.29196E+01
   Friction thermal sca.    tstar :  0.12156E+01 0.18924E+03
   Rough dim-less th. sca.  tplus :  0.65634E-02 0.20682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27093E+00      10   0.15164E-04   0.50741E+01 0.36616E+02 
c  Velocity[X]                                      0.22188E+01 
c  Velocity[Y]                                      0.12824E+01 
c  Velocity[Z]                                      0.15729E+01 
c  Pressure     0.17937E-04      19   0.31845E-03   0.18349E-01 0.36673E+02 
c  k            0.20294E-01      13   0.89083E-04   0.16464E+00 0.56850E+02 
c  omega        0.27922E+07       1   0.96023E-07   0.16313E+08 0.70043E+00 
c  TempK        0.10045E+05       4   0.49371E-05   0.50124E+01 0.82143E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3267e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.122          19.245      0.00069496       -0.013581
v  Velocity[Y]             -15.514          15.437         0.28893         0.41757
v  Velocity[Z]             -25.435          11.973         -1.6377        -0.50825
v  ǁVelocityǁ         0.00016672          25.605          7.6552           6.531
v  Pressure                -563.28          201.21          25.505          30.654
v  k                   9.8035e-011          9.3493         0.24151         0.52672
v  omega                    57.496     2.7317e+008     1.2912e+006           76855
v  TempK                    298.57          363.17          337.83          346.63
v  TurbVisc            2.4568e-018       0.0021135     6.1641e-005      0.00021763
v  CourantNb            0.00014647          1.5806         0.78901         0.96996
v  FourierNb              0.003814               1         0.42017         0.18736
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006        0.004782      7.418e-005      0.00020371

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.5          306.58
v  Yplus               0          2.9196         0.62862          0.4837


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45643          2.1757          1.2092          1.1573


 INSTANT    0.850000000E-02   TIME STEP NUMBER             850
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925281E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13517E-01 0.46678E+01
   Friction velocity        uk    :  0.13517E-01 0.46639E+01
   Dimensionless distance   yplus :  0.91646E-02 0.29199E+01
   Friction thermal sca.    tstar :  0.12155E+01 0.19132E+03
   Rough dim-less th. sca.  tplus :  0.64922E-02 0.20685E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27091E+00      10   0.15199E-04   0.50909E+01 0.36602E+02 
c  Velocity[X]                                      0.22225E+01 
c  Velocity[Y]                                      0.12855E+01 
c  Velocity[Z]                                      0.15829E+01 
c  Pressure     0.18175E-04      19   0.31758E-03   0.18591E-01 0.36448E+02 
c  k            0.20304E-01      13   0.89452E-04   0.16675E+00 0.57085E+02 
c  omega        0.27922E+07       1   0.93124E-07   0.80405E+07 0.55268E+00 
c  TempK        0.10045E+05       4   0.49328E-05   0.50080E+01 0.82091E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.328e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.125          19.244      0.00065614        -0.01362
v  Velocity[Y]             -15.452          15.435         0.28928          0.4184
v  Velocity[Z]              -25.43           11.97         -1.6376        -0.50824
v  ǁVelocityǁ          0.0001672          25.604          7.6548          6.5305
v  Pressure                -563.44          200.99          25.296          30.451
v  k                   9.8026e-011          9.3583         0.24167         0.52708
v  omega                    57.496     2.7317e+008     1.2912e+006           76855
v  TempK                    298.57          363.17          337.84          346.64
v  TurbVisc            2.4566e-018       0.0021173     6.1693e-005      0.00021781
v  CourantNb            0.00016129          1.5803         0.78899         0.96995
v  FourierNb             0.0038139               1         0.42022         0.18746
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0048572      7.418e-005       0.0002037

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.5          306.58
v  Yplus               0          2.9199          0.6286         0.48367


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.34161          2.1753          1.2092          1.1574


 INSTANT    0.851000000E-02   TIME STEP NUMBER             851
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925322E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13374E-01 0.46679E+01
   Friction velocity        uk    :  0.13374E-01 0.46639E+01
   Dimensionless distance   yplus :  0.90678E-02 0.29203E+01
   Friction thermal sca.    tstar :  0.12152E+01 0.19336E+03
   Rough dim-less th. sca.  tplus :  0.64237E-02 0.20688E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27088E+00      10   0.15305E-04   0.51078E+01 0.36619E+02 
c  Velocity[X]                                      0.22203E+01 
c  Velocity[Y]                                      0.12925E+01 
c  Velocity[Z]                                      0.15950E+01 
c  Pressure     0.18289E-04      19   0.31124E-03   0.18710E-01 0.37023E+02 
c  k            0.20313E-01      13   0.89765E-04   0.16874E+00 0.57301E+02 
c  omega        0.27922E+07       1   0.93150E-07   0.80191E+07 0.55239E+00 
c  TempK        0.10044E+05       4   0.49289E-05   0.50038E+01 0.82037E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3291e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.127          19.244      0.00061686       -0.013659
v  Velocity[Y]             -15.442          15.432         0.28963         0.41922
v  Velocity[Z]             -25.425          11.967         -1.6376        -0.50824
v  ǁVelocityǁ         0.00016803          25.603          7.6544          6.5301
v  Pressure                -563.61          200.77          25.083          30.244
v  k                   9.8017e-011          9.3628         0.24182         0.52744
v  omega                    57.496     2.7317e+008     1.2912e+006           76854
v  TempK                    298.57          363.17          337.84          346.65
v  TurbVisc            2.4564e-018       0.0021207     6.1745e-005      0.00021799
v  CourantNb            0.00017559            1.58         0.78897         0.96993
v  FourierNb             0.0038138               1         0.42027         0.18757
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0049296     7.4179e-005       0.0002037

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.5          306.58
v  Yplus               0          2.9203         0.62858         0.48365


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65607          2.1751          1.2092          1.1575


 INSTANT    0.852000000E-02   TIME STEP NUMBER             852
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925296E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13223E-01 0.46679E+01
   Friction velocity        uk    :  0.13223E-01 0.46640E+01
   Dimensionless distance   yplus :  0.89655E-02 0.29207E+01
   Friction thermal sca.    tstar :  0.12153E+01 0.19557E+03
   Rough dim-less th. sca.  tplus :  0.63512E-02 0.20691E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27085E+00      10   0.15473E-04   0.51223E+01 0.36649E+02 
c  Velocity[X]                                      0.22184E+01 
c  Velocity[Y]                                      0.12997E+01 
c  Velocity[Z]                                      0.16042E+01 
c  Pressure     0.18167E-04      19   0.31000E-03   0.18586E-01 0.36617E+02 
c  k            0.20322E-01      13   0.89918E-04   0.17092E+00 0.57516E+02 
c  omega        0.27922E+07       1   0.94254E-07   0.10422E+08 0.59476E+00 
c  TempK        0.10044E+05       4   0.49252E-05   0.50020E+01 0.81988E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step       6.33e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.13          19.244      0.00057434         -0.0137
v  Velocity[Y]             -15.535           15.43         0.28998         0.42003
v  Velocity[Z]              -25.42          11.964         -1.6376        -0.50823
v  ǁVelocityǁ         0.00016914          25.603           7.654          6.5296
v  Pressure                -563.79          200.55          24.874           30.04
v  k                   9.8007e-011          9.3636         0.24198         0.52779
v  omega                    57.496     2.7317e+008     1.2912e+006           76854
v  TempK                    298.57          363.17          337.85          346.66
v  TurbVisc            2.4562e-018       0.0021218     6.1797e-005      0.00021816
v  CourantNb            0.00018933          1.5798         0.78895         0.96992
v  FourierNb             0.0038137               1         0.42031         0.18768
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0136e+005
v  Local Time Step          1e-006       0.0050028     7.4179e-005      0.00020369

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.5          306.58
v  Yplus               0          2.9207         0.62857         0.48363


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66085          2.1749          1.2093          1.1576


 INSTANT    0.853000000E-02   TIME STEP NUMBER             853
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925316E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13084E-01 0.46679E+01
   Friction velocity        uk    :  0.13084E-01 0.46640E+01
   Dimensionless distance   yplus :  0.88710E-02 0.29211E+01
   Friction thermal sca.    tstar :  0.12153E+01 0.19765E+03
   Rough dim-less th. sca.  tplus :  0.62843E-02 0.20693E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27083E+00      10   0.15951E-04   0.51409E+01 0.36700E+02 
c  Velocity[X]                                      0.22183E+01 
c  Velocity[Y]                                      0.13086E+01 
c  Velocity[Z]                                      0.16139E+01 
c  Pressure     0.18055E-04      19   0.32610E-03   0.18474E-01 0.37216E+02 
c  k            0.20330E-01      13   0.89953E-04   0.17336E+00 0.57732E+02 
c  omega        0.27922E+07       1   0.97963E-07   0.21349E+08 0.76884E+00 
c  TempK        0.10044E+05       4   0.49221E-05   0.50059E+01 0.81970E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3308e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.133          19.243      0.00053275       -0.013741
v  Velocity[Y]             -15.589          15.427         0.29033         0.42084
v  Velocity[Z]             -25.415          11.961         -1.6376        -0.50823
v  ǁVelocityǁ          0.0001705          25.602          7.6535          6.5291
v  Pressure                -563.98          200.33          24.662          29.832
v  k                   9.7998e-011          9.3616         0.24213         0.52813
v  omega                    57.496     2.7317e+008     1.2912e+006           76854
v  TempK                    298.57          363.17          337.85          346.67
v  TurbVisc            2.4559e-018       0.0021202     6.1848e-005      0.00021833
v  CourantNb            0.00019632          1.5796         0.78893         0.96991
v  FourierNb             0.0038136               1         0.42036         0.18779
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0050785     7.4179e-005      0.00020369

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.5          306.58
v  Yplus               0          2.9211         0.62855         0.48361


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53304          2.1747          1.2093          1.1577


 INSTANT    0.854000000E-02   TIME STEP NUMBER             854
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925356E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12907E-01 0.46680E+01
   Friction velocity        uk    :  0.12907E-01 0.46641E+01
   Dimensionless distance   yplus :  0.87514E-02 0.29215E+01
   Friction thermal sca.    tstar :  0.12155E+01 0.20036E+03
   Rough dim-less th. sca.  tplus :  0.61995E-02 0.20696E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27080E+00      10   0.16038E-04   0.51625E+01 0.36757E+02 
c  Velocity[X]                                      0.22182E+01 
c  Velocity[Y]                                      0.13218E+01 
c  Velocity[Z]                                      0.16225E+01 
c  Pressure     0.18046E-04      18   0.32973E-03   0.18468E-01 0.37476E+02 
c  k            0.20338E-01      13   0.90198E-04   0.17608E+00 0.57920E+02 
c  omega        0.27922E+07       1   0.96709E-07   0.18262E+08 0.72416E+00 
c  TempK        0.10044E+05       4   0.49191E-05   0.50111E+01 0.81928E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3325e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.135          19.243      0.00049093        -0.01378
v  Velocity[Y]             -15.517          15.424         0.29068         0.42165
v  Velocity[Z]              -25.41          11.958         -1.6375        -0.50823
v  ǁVelocityǁ         0.00017191          25.601          7.6531          6.5286
v  Pressure                -564.17          200.11          24.448          29.624
v  k                   9.7988e-011          9.3575         0.24229         0.52846
v  omega                    57.495     2.7317e+008     1.2912e+006           76854
v  TempK                    298.57          363.17          337.86          346.68
v  TurbVisc            2.4557e-018       0.0021157     6.1899e-005       0.0002185
v  CourantNb            0.00019618          1.5791         0.78891          0.9699
v  FourierNb             0.0038135               1         0.42041         0.18789
v  total_pressure      1.0076e+005     1.0153e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0051566     7.4179e-005      0.00020368

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.5          306.59
v  Yplus               0          2.9215         0.62853         0.48358


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45579          2.1743          1.2093          1.1578


 INSTANT    0.855000000E-02   TIME STEP NUMBER             855
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925406E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12732E-01 0.46680E+01
   Friction velocity        uk    :  0.12732E-01 0.46641E+01
   Dimensionless distance   yplus :  0.86324E-02 0.29219E+01
   Friction thermal sca.    tstar :  0.12156E+01 0.20312E+03
   Rough dim-less th. sca.  tplus :  0.61153E-02 0.20699E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27078E+00      10   0.16083E-04   0.51701E+01 0.36722E+02 
c  Velocity[X]                                      0.22166E+01 
c  Velocity[Y]                                      0.13226E+01 
c  Velocity[Z]                                      0.16309E+01 
c  Pressure     0.18159E-04      18   0.32361E-03   0.18590E-01 0.40390E+02 
c  k            0.20346E-01      13   0.90340E-04   0.17863E+00 0.58053E+02 
c  omega        0.27922E+07       1   0.94607E-07   0.11867E+08 0.61894E+00 
c  TempK        0.10044E+05       4   0.49160E-05   0.50169E+01 0.81900E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3344e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.137          19.242      0.00044918        -0.01382
v  Velocity[Y]             -15.459          15.421         0.29103         0.42246
v  Velocity[Z]             -25.404          11.954         -1.6375        -0.50822
v  ǁVelocityǁ         0.00017337            25.6          7.6527          6.5282
v  Pressure                -564.39          199.86          24.215          29.397
v  k                   9.7979e-011           9.352         0.24244         0.52879
v  omega                    57.495     2.7317e+008     1.2912e+006           76854
v  TempK                    298.56          363.17          337.86          346.69
v  TurbVisc            2.4554e-018       0.0021111      6.195e-005      0.00021866
v  CourantNb            0.00019609          1.5787         0.78889         0.96989
v  FourierNb             0.0038133               1         0.42046         0.18799
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0052368     7.4179e-005      0.00020368

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.5          306.59
v  Yplus               0          2.9219         0.62851         0.48356


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54738          2.1738          1.2093          1.1579


 INSTANT    0.856000000E-02   TIME STEP NUMBER             856
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925274E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12588E-01 0.46681E+01
   Friction velocity        uk    :  0.12588E-01 0.46641E+01
   Dimensionless distance   yplus :  0.85351E-02 0.29223E+01
   Friction thermal sca.    tstar :  0.12155E+01 0.20544E+03
   Rough dim-less th. sca.  tplus :  0.60463E-02 0.20702E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27075E+00      10   0.16124E-04   0.51796E+01 0.36709E+02 
c  Velocity[X]                                      0.22140E+01 
c  Velocity[Y]                                      0.13274E+01 
c  Velocity[Z]                                      0.16382E+01 
c  Pressure     0.18280E-04      19   0.31840E-03   0.18719E-01 0.39385E+02 
c  k            0.20353E-01      13   0.90387E-04   0.18083E+00 0.58134E+02 
c  omega        0.27922E+07       1   0.93155E-07   0.82610E+07 0.55074E+00 
c  TempK        0.10044E+05       4   0.49131E-05   0.50228E+01 0.81869E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3361e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.139          19.242      0.00040508       -0.013861
v  Velocity[Y]             -15.453          15.418         0.29138         0.42326
v  Velocity[Z]             -25.399          11.951         -1.6375         -0.5082
v  ǁVelocityǁ         0.00017488          25.599          7.6523          6.5277
v  Pressure                -564.59          199.63           23.99          29.177
v  k                   9.7969e-011          9.3453         0.24259          0.5291
v  omega                    57.495     2.7317e+008     1.2912e+006           76853
v  TempK                    298.56          363.17          337.87           346.7
v  TurbVisc            2.4552e-018       0.0021061        6.2e-005      0.00021882
v  CourantNb            0.00019597          1.5783         0.78887         0.96987
v  FourierNb             0.0038132               1          0.4205         0.18809
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0053167      7.418e-005      0.00020367

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.5          306.59
v  Yplus               0          2.9223         0.62849         0.48354


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.34592          2.1734          1.2094           1.158


 INSTANT    0.857000000E-02   TIME STEP NUMBER             857
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925339E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12436E-01 0.46681E+01
   Friction velocity        uk    :  0.12436E-01 0.46642E+01
   Dimensionless distance   yplus :  0.84320E-02 0.29227E+01
   Friction thermal sca.    tstar :  0.12154E+01 0.20795E+03
   Rough dim-less th. sca.  tplus :  0.59733E-02 0.20704E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27073E+00      10   0.16083E-04   0.51912E+01 0.36734E+02 
c  Velocity[X]                                      0.22111E+01 
c  Velocity[Y]                                      0.13350E+01 
c  Velocity[Z]                                      0.16452E+01 
c  Pressure     0.18182E-04      18   0.31864E-03   0.18623E-01 0.40175E+02 
c  k            0.20361E-01      13   0.90388E-04   0.18260E+00 0.58171E+02 
c  omega        0.27922E+07       1   0.94282E-07   0.10375E+08 0.58620E+00 
c  TempK        0.10044E+05       4   0.49104E-05   0.50269E+01 0.81827E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3375e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.141          19.242      0.00036117       -0.013901
v  Velocity[Y]             -15.558          15.415         0.29172         0.42407
v  Velocity[Z]             -25.393          11.948         -1.6375        -0.50819
v  ǁVelocityǁ         0.00017649          25.598          7.6519          6.5273
v  Pressure                -564.78           199.4           23.76          28.953
v  k                   9.7959e-011          9.3377         0.24273         0.52941
v  omega                    57.495     2.7317e+008     1.2912e+006           76853
v  TempK                    298.56          363.17          337.88          346.71
v  TurbVisc             2.455e-018       0.0020989      6.205e-005      0.00021897
v  CourantNb            0.00019585          1.5779         0.78885         0.96986
v  FourierNb             0.0038131               1         0.42055         0.18819
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0053907     7.4182e-005      0.00020367

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.5          306.59
v  Yplus               0          2.9227         0.62848         0.48352


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38558          2.1731          1.2094           1.158


 INSTANT    0.858000000E-02   TIME STEP NUMBER             858
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925280E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12269E-01 0.46682E+01
   Friction velocity        uk    :  0.12269E-01 0.46642E+01
   Dimensionless distance   yplus :  0.83188E-02 0.29230E+01
   Friction thermal sca.    tstar :  0.12154E+01 0.21078E+03
   Rough dim-less th. sca.  tplus :  0.58931E-02 0.20707E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27070E+00      10   0.15949E-04   0.52055E+01 0.36762E+02 
c  Velocity[X]                                      0.22084E+01 
c  Velocity[Y]                                      0.13447E+01 
c  Velocity[Z]                                      0.16524E+01 
c  Pressure     0.18198E-04      19   0.31622E-03   0.18644E-01 0.40388E+02 
c  k            0.20368E-01      13   0.89824E-04   0.18387E+00 0.58175E+02 
c  omega        0.27922E+07       1   0.99007E-07   0.24778E+08 0.81454E+00 
c  TempK        0.10044E+05       4   0.49081E-05   0.50268E+01 0.81785E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.339e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.143          19.242      0.00031829        -0.01394
v  Velocity[Y]             -15.611          15.411         0.29207         0.42487
v  Velocity[Z]             -25.388          11.945         -1.6375        -0.50817
v  ǁVelocityǁ         0.00017804          25.597          7.6514          6.5269
v  Pressure                -564.96          199.16           23.53          28.727
v  k                   9.7949e-011          9.3295         0.24288         0.52971
v  omega                    57.495     2.7317e+008     1.2912e+006           76853
v  TempK                    298.56          363.17          337.88          346.72
v  TurbVisc            2.4547e-018       0.0020896       6.21e-005      0.00021912
v  CourantNb            0.00019572          1.5775         0.78883         0.96985
v  FourierNb             0.0038129               1          0.4206         0.18828
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0054635     7.4183e-005      0.00020366

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.5          306.59
v  Yplus               0           2.923         0.62846          0.4835


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44326          2.1727          1.2094          1.1581


 INSTANT    0.859000000E-02   TIME STEP NUMBER             859
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925331E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12117E-01 0.46682E+01
   Friction velocity        uk    :  0.12117E-01 0.46643E+01
   Dimensionless distance   yplus :  0.82157E-02 0.29234E+01
   Friction thermal sca.    tstar :  0.12153E+01 0.21343E+03
   Rough dim-less th. sca.  tplus :  0.58200E-02 0.20710E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27068E+00      10   0.16278E-04   0.52176E+01 0.36779E+02 
c  Velocity[X]                                      0.22050E+01 
c  Velocity[Y]                                      0.13545E+01 
c  Velocity[Z]                                      0.16580E+01 
c  Pressure     0.18383E-04      19   0.31854E-03   0.18837E-01 0.41380E+02 
c  k            0.20375E-01      13   0.88752E-04   0.18448E+00 0.58130E+02 
c  omega        0.27922E+07       1   0.95998E-07   0.15788E+08 0.68327E+00 
c  TempK        0.10044E+05       4   0.49059E-05   0.50262E+01 0.81726E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3413e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.145          19.242       0.0002739       -0.013976
v  Velocity[Y]             -15.526          15.408         0.29241         0.42567
v  Velocity[Z]             -25.382          11.942         -1.6374        -0.50815
v  ǁVelocityǁ         0.00017945          25.596           7.651          6.5264
v  Pressure                -565.15          198.91          23.292          28.495
v  k                   9.7939e-011          9.3207         0.24303         0.53001
v  omega                    57.495     2.7317e+008     1.2912e+006           76853
v  TempK                    298.56          363.17          337.89          346.72
v  TurbVisc            2.4545e-018        0.002078     6.2151e-005      0.00021928
v  CourantNb            0.00019564           1.577         0.78881         0.96984
v  FourierNb             0.0038128               1         0.42065         0.18838
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.005541     7.4185e-005      0.00020365

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17           305.5          306.59
v  Yplus               0          2.9234         0.62845         0.48348


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56187          2.1722          1.2095          1.1582


 INSTANT    0.860000000E-02   TIME STEP NUMBER             860
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925317E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11958E-01 0.46683E+01
   Friction velocity        uk    :  0.11958E-01 0.46644E+01
   Dimensionless distance   yplus :  0.81074E-02 0.29238E+01
   Friction thermal sca.    tstar :  0.12153E+01 0.21628E+03
   Rough dim-less th. sca.  tplus :  0.57434E-02 0.20712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27066E+00      10   0.16398E-04   0.52276E+01 0.36773E+02 
c  Velocity[X]                                      0.22024E+01 
c  Velocity[Y]                                      0.13582E+01 
c  Velocity[Z]                                      0.16670E+01 
c  Pressure     0.18484E-04      19   0.31615E-03   0.18945E-01 0.41864E+02 
c  k            0.20381E-01      13   0.88074E-04   0.18515E+00 0.58080E+02 
c  omega        0.27922E+07       1   0.94764E-07   0.10793E+08 0.59332E+00 
c  TempK        0.10044E+05       4   0.49036E-05   0.50324E+01 0.81709E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3438e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.147          19.242      0.00022724       -0.014009
v  Velocity[Y]             -15.464          15.404         0.29276         0.42647
v  Velocity[Z]             -25.376          11.938         -1.6374        -0.50814
v  ǁVelocityǁ         0.00018048          25.595          7.6506           6.526
v  Pressure                -565.33          198.66          23.053          28.261
v  k                   9.7929e-011          9.3115         0.24318          0.5303
v  omega                    57.495     2.7317e+008     1.2912e+006           76853
v  TempK                    298.56          363.17          337.89          346.73
v  TurbVisc            2.4542e-018       0.0020643     6.2201e-005      0.00021942
v  CourantNb            0.00019555          1.5763         0.78878         0.96982
v  FourierNb             0.0038126               1          0.4207         0.18847
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0056021     7.4187e-005      0.00020365

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0          2.9238         0.62843         0.48346


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49877          2.1716          1.2095          1.1583


 INSTANT    0.861000000E-02   TIME STEP NUMBER             861
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925352E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11753E-01 0.46683E+01
   Friction velocity        uk    :  0.11753E-01 0.46644E+01
   Dimensionless distance   yplus :  0.79689E-02 0.29242E+01
   Friction thermal sca.    tstar :  0.12154E+01 0.22005E+03
   Rough dim-less th. sca.  tplus :  0.56452E-02 0.20715E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27063E+00      10   0.16349E-04   0.52494E+01 0.36829E+02 
c  Velocity[X]                                      0.22039E+01 
c  Velocity[Y]                                      0.13714E+01 
c  Velocity[Z]                                      0.16741E+01 
c  Pressure     0.18831E-04      20   0.31851E-03   0.19307E-01 0.42100E+02 
c  k            0.20388E-01      13   0.87466E-04   0.18589E+00 0.58022E+02 
c  omega        0.27922E+07       1   0.96986E-07   0.17383E+08 0.71050E+00 
c  TempK        0.10044E+05       4   0.49013E-05   0.50402E+01 0.81703E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3461e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.148          19.242      0.00018074       -0.014037
v  Velocity[Y]             -15.454          15.401         0.29311         0.42726
v  Velocity[Z]              -25.37          11.935         -1.6374        -0.50812
v  ǁVelocityǁ         0.00018121          25.594          7.6502          6.5256
v  Pressure                -565.49          198.42          22.812          28.025
v  k                    9.792e-011          9.3017         0.24332         0.53058
v  omega                    57.495     2.7317e+008     1.2912e+006           76853
v  TempK                    298.56          363.17           337.9          346.74
v  TurbVisc             2.454e-018       0.0020486      6.225e-005      0.00021957
v  CourantNb            0.00019552          1.5758         0.78876         0.96981
v  FourierNb             0.0038125               1         0.42075         0.18856
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0056494     7.4189e-005      0.00020364

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0          2.9242         0.62841         0.48344


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56377           2.171          1.2095          1.1584


 INSTANT    0.862000000E-02   TIME STEP NUMBER             862
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925361E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11569E-01 0.46684E+01
   Friction velocity        uk    :  0.11569E-01 0.46645E+01
   Dimensionless distance   yplus :  0.78441E-02 0.29245E+01
   Friction thermal sca.    tstar :  0.12155E+01 0.22355E+03
   Rough dim-less th. sca.  tplus :  0.55568E-02 0.20718E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27061E+00      10   0.16219E-04   0.52690E+01 0.36864E+02 
c  Velocity[X]                                      0.22065E+01 
c  Velocity[Y]                                      0.13801E+01 
c  Velocity[Z]                                      0.16824E+01 
c  Pressure     0.18917E-04      19   0.31924E-03   0.19399E-01 0.43703E+02 
c  k            0.20394E-01      13   0.86651E-04   0.18670E+00 0.57952E+02 
c  omega        0.27922E+07       1   0.96202E-07   0.12889E+08 0.63248E+00 
c  TempK        0.10044E+05       4   0.48988E-05   0.50408E+01 0.81677E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3482e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.15          19.242      0.00013098       -0.014062
v  Velocity[Y]              -15.55          15.397         0.29345         0.42805
v  Velocity[Z]             -25.364          11.932         -1.6374        -0.50811
v  ǁVelocityǁ         0.00018137          25.594          7.6498          6.5252
v  Pressure                -565.64          198.16          22.562           27.78
v  k                    9.791e-011          9.2916         0.24347         0.53085
v  omega                    57.495     2.7317e+008     1.2912e+006           76852
v  TempK                    298.56          363.17           337.9          346.75
v  TurbVisc            2.4537e-018       0.0020308     6.2298e-005      0.00021971
v  CourantNb            0.00019547          1.5752         0.78874          0.9698
v  FourierNb             0.0038123               1          0.4208         0.18865
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0056928     7.4193e-005      0.00020364

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0          2.9245          0.6284         0.48342


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50921          2.1705          1.2095          1.1585


 INSTANT    0.863000000E-02   TIME STEP NUMBER             863
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925308E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11414E-01 0.46685E+01
   Friction velocity        uk    :  0.11414E-01 0.46646E+01
   Dimensionless distance   yplus :  0.77391E-02 0.29249E+01
   Friction thermal sca.    tstar :  0.12154E+01 0.22658E+03
   Rough dim-less th. sca.  tplus :  0.54824E-02 0.20720E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27059E+00      10   0.16252E-04   0.52872E+01 0.36911E+02 
c  Velocity[X]                                      0.22064E+01 
c  Velocity[Y]                                      0.13893E+01 
c  Velocity[Z]                                      0.16914E+01 
c  Pressure     0.19002E-04      19   0.31920E-03   0.19492E-01 0.42662E+02 
c  k            0.20400E-01      13   0.85618E-04   0.18634E+00 0.57805E+02 
c  omega        0.27922E+07       1   0.10058E-06   0.25603E+08 0.82688E+00 
c  TempK        0.10044E+05       4   0.48964E-05   0.50464E+01 0.81687E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3504e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.151          19.242     8.4863e-005       -0.014081
v  Velocity[Y]             -15.594          15.393         0.29379         0.42884
v  Velocity[Z]             -25.358          11.929         -1.6374        -0.50808
v  ǁVelocityǁ          0.0001813          25.592          7.6494          6.5249
v  Pressure                -565.77          197.91          22.319          27.542
v  k                     9.79e-011           9.281         0.24361         0.53112
v  omega                    57.495     2.7317e+008     1.2912e+006           76852
v  TempK                    298.56          363.17          337.91          346.76
v  TurbVisc            2.4535e-018        0.002011     6.2346e-005      0.00021985
v  CourantNb            0.00019547          1.5747         0.78872         0.96979
v  FourierNb             0.0038122               1         0.42085         0.18874
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0057364     7.4195e-005      0.00020363

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0          2.9249         0.62838          0.4834


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56776            2.17          1.2096          1.1585


 INSTANT    0.864000000E-02   TIME STEP NUMBER             864
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925346E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11252E-01 0.46686E+01
   Friction velocity        uk    :  0.11252E-01 0.46646E+01
   Dimensionless distance   yplus :  0.76289E-02 0.29252E+01
   Friction thermal sca.    tstar :  0.12153E+01 0.22986E+03
   Rough dim-less th. sca.  tplus :  0.54044E-02 0.20723E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27056E+00      10   0.16295E-04   0.53059E+01 0.36960E+02 
c  Velocity[X]                                      0.22075E+01 
c  Velocity[Y]                                      0.14009E+01 
c  Velocity[Z]                                      0.16974E+01 
c  Pressure     0.18874E-04      19   0.32856E-03   0.19366E-01 0.43592E+02 
c  k            0.20406E-01      13   0.84440E-04   0.18587E+00 0.57680E+02 
c  omega        0.27922E+07       1   0.97923E-07   0.17211E+08 0.70967E+00 
c  TempK        0.10045E+05       4   0.48939E-05   0.50463E+01 0.81653E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3534e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.152          19.242     3.8641e-005       -0.014097
v  Velocity[Y]             -15.503          15.389         0.29413         0.42962
v  Velocity[Z]             -25.352          11.925         -1.6374        -0.50806
v  ǁVelocityǁ         0.00018065          25.591           7.649          6.5245
v  Pressure                 -565.9          197.66          22.071          27.299
v  k                    9.789e-011            9.27         0.24375         0.53138
v  omega                    57.495     2.7317e+008     1.2912e+006           76852
v  TempK                    298.55          363.17          337.91          346.77
v  TurbVisc            2.4532e-018        0.001999     6.2394e-005      0.00021998
v  CourantNb            0.00019541           1.574          0.7887         0.96978
v  FourierNb              0.003812               1         0.42089         0.18882
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0057792     7.4196e-005      0.00020362

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0          2.9252         0.62837         0.48338


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50168          2.1693          1.2096          1.1586


 INSTANT    0.865000000E-02   TIME STEP NUMBER             865
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925331E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11087E-01 0.46686E+01
   Friction velocity        uk    :  0.11087E-01 0.46647E+01
   Dimensionless distance   yplus :  0.75169E-02 0.29256E+01
   Friction thermal sca.    tstar :  0.12153E+01 0.23329E+03
   Rough dim-less th. sca.  tplus :  0.53250E-02 0.20725E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27054E+00      10   0.16444E-04   0.53172E+01 0.36962E+02 
c  Velocity[X]                                      0.22103E+01 
c  Velocity[Y]                                      0.14045E+01 
c  Velocity[Z]                                      0.17025E+01 
c  Pressure     0.18978E-04      20   0.33918E-03   0.19478E-01 0.44181E+02 
c  k            0.20412E-01      13   0.83116E-04   0.18541E+00 0.57559E+02 
c  omega        0.27922E+07       1   0.95539E-07   0.90610E+07 0.57026E+00 
c  TempK        0.10045E+05       4   0.48912E-05   0.50452E+01 0.81612E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3566e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.154          19.242    -6.1271e-006       -0.014112
v  Velocity[Y]             -15.427          15.385         0.29446         0.43041
v  Velocity[Z]             -25.347          11.922         -1.6374        -0.50804
v  ǁVelocityǁ         0.00017934           25.59          7.6486          6.5241
v  Pressure                -566.03           197.4           21.82          27.053
v  k                    9.788e-011          9.2585          0.2439         0.53164
v  omega                    57.495     2.7318e+008     1.2912e+006           76852
v  TempK                    298.55          363.17          337.92          346.78
v  TurbVisc             2.453e-018       0.0019873     6.2441e-005      0.00022011
v  CourantNb            0.00019545          1.5732         0.78868         0.96976
v  FourierNb             0.0038118               1         0.42094          0.1889
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.005821     7.4196e-005      0.00020361

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0          2.9256         0.62835         0.48336


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5044          2.1685          1.2096          1.1587


 INSTANT    0.866000000E-02   TIME STEP NUMBER             866
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925261E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10925E-01 0.46687E+01
   Friction velocity        uk    :  0.10925E-01 0.46648E+01
   Dimensionless distance   yplus :  0.74076E-02 0.29260E+01
   Friction thermal sca.    tstar :  0.12152E+01 0.23673E+03
   Rough dim-less th. sca.  tplus :  0.52476E-02 0.20728E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27052E+00      10   0.16437E-04   0.53318E+01 0.36995E+02 
c  Velocity[X]                                      0.22144E+01 
c  Velocity[Y]                                      0.14135E+01 
c  Velocity[Z]                                      0.17040E+01 
c  Pressure     0.19076E-04      19   0.33241E-03   0.19585E-01 0.44092E+02 
c  k            0.20418E-01      13   0.81757E-04   0.18438E+00 0.57301E+02 
c  omega        0.27922E+07       1   0.95748E-07   0.88154E+07 0.56910E+00 
c  TempK        0.10045E+05       4   0.48883E-05   0.50409E+01 0.81565E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3594e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.155          19.242     -4.716e-005       -0.014123
v  Velocity[Y]             -15.399          15.381         0.29479         0.43118
v  Velocity[Z]             -25.341          11.918         -1.6374        -0.50802
v  ǁVelocityǁ         0.00017722          25.589          7.6482          6.5238
v  Pressure                -566.13          197.14          21.569          26.807
v  k                    9.787e-011          9.2465         0.24404         0.53189
v  omega                    57.495     2.7318e+008     1.2912e+006           76852
v  TempK                    298.55          363.17          337.92          346.79
v  TurbVisc            2.4527e-018        0.001974     6.2487e-005      0.00022023
v  CourantNb             0.0001955          1.5725         0.78866         0.96975
v  FourierNb             0.0038117               1         0.42098         0.18897
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0057139     7.4196e-005       0.0002036

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0           2.926         0.62834         0.48334


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46264          2.1679          1.2096          1.1587


 INSTANT    0.867000000E-02   TIME STEP NUMBER             867
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925306E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10748E-01 0.46688E+01
   Friction velocity        uk    :  0.10748E-01 0.46649E+01
   Dimensionless distance   yplus :  0.72873E-02 0.29263E+01
   Friction thermal sca.    tstar :  0.12151E+01 0.24064E+03
   Rough dim-less th. sca.  tplus :  0.51624E-02 0.20730E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27049E+00      10   0.16446E-04   0.53482E+01 0.37042E+02 
c  Velocity[X]                                      0.22168E+01 
c  Velocity[Y]                                      0.14228E+01 
c  Velocity[Z]                                      0.17086E+01 
c  Pressure     0.19636E-04      19   0.33638E-03   0.20165E-01 0.43686E+02 
c  k            0.20423E-01      13   0.80339E-04   0.18334E+00 0.57037E+02 
c  omega        0.27922E+07       1   0.97165E-07   0.11877E+08 0.62229E+00 
c  TempK        0.10045E+05       4   0.48857E-05   0.50375E+01 0.81523E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3621e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.156          19.241    -8.7217e-005       -0.014134
v  Velocity[Y]             -15.441          15.377         0.29512         0.43196
v  Velocity[Z]             -25.335          11.915         -1.6374          -0.508
v  ǁVelocityǁ         0.00017464          25.589          7.6478          6.5234
v  Pressure                -566.22          196.89          21.321          26.564
v  k                    9.786e-011           9.234         0.24418         0.53213
v  omega                    57.495     2.7318e+008     1.2912e+006           76852
v  TempK                    298.55          363.17          337.93           346.8
v  TurbVisc            2.4525e-018       0.0019591     6.2532e-005      0.00022035
v  CourantNb            0.00019561          1.5718         0.78864         0.96974
v  FourierNb             0.0038115               1         0.42103         0.18905
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.005187     7.4196e-005      0.00020359

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0          2.9263         0.62833         0.48332


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54128          2.1672          1.2097          1.1588


 INSTANT    0.868000000E-02   TIME STEP NUMBER             868
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925368E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10595E-01 0.46689E+01
   Friction velocity        uk    :  0.10595E-01 0.46650E+01
   Dimensionless distance   yplus :  0.71836E-02 0.29267E+01
   Friction thermal sca.    tstar :  0.12152E+01 0.24412E+03
   Rough dim-less th. sca.  tplus :  0.50889E-02 0.20733E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27047E+00      10   0.16398E-04   0.53686E+01 0.37138E+02 
c  Velocity[X]                                      0.22184E+01 
c  Velocity[Y]                                      0.14355E+01 
c  Velocity[Z]                                      0.17146E+01 
c  Pressure     0.19587E-04      19   0.34307E-03   0.20119E-01 0.43445E+02 
c  k            0.20429E-01      13   0.79135E-04   0.18245E+00 0.56800E+02 
c  omega        0.27922E+07       1   0.10152E-06   0.21266E+08 0.77161E+00 
c  TempK        0.10045E+05       4   0.48835E-05   0.50393E+01 0.81497E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3645e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.156          19.241     -0.00012361       -0.014143
v  Velocity[Y]              -15.51          15.372         0.29544         0.43273
v  Velocity[Z]             -25.329          11.911         -1.6374        -0.50798
v  ǁVelocityǁ         0.00017137          25.588          7.6474          6.5231
v  Pressure                -566.28          196.64          21.076          26.323
v  k                    9.785e-011           9.221         0.24432         0.53237
v  omega                    57.495     2.7318e+008     1.2912e+006           76851
v  TempK                    298.55          363.17          337.93          346.81
v  TurbVisc            2.4522e-018       0.0019479     6.2577e-005      0.00022047
v  CourantNb            0.00019566          1.5712         0.78862         0.96972
v  FourierNb             0.0038113               1         0.42107         0.18912
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0047746     7.4196e-005      0.00020358

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0          2.9267         0.62832          0.4833


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44495          2.1667          1.2097          1.1588


 INSTANT    0.869000000E-02   TIME STEP NUMBER             869
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925325E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10371E-01 0.46690E+01
   Friction velocity        uk    :  0.10371E-01 0.46651E+01
   Dimensionless distance   yplus :  0.70318E-02 0.29270E+01
   Friction thermal sca.    tstar :  0.12153E+01 0.24939E+03
   Rough dim-less th. sca.  tplus :  0.49813E-02 0.20735E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27045E+00      10   0.16282E-04   0.53838E+01 0.37209E+02 
c  Velocity[X]                                      0.22217E+01 
c  Velocity[Y]                                      0.14478E+01 
c  Velocity[Z]                                      0.17143E+01 
c  Pressure     0.19023E-04      19   0.33815E-03   0.19543E-01 0.44353E+02 
c  k            0.20435E-01      13   0.78632E-04   0.18136E+00 0.56558E+02 
c  omega        0.27922E+07       1   0.10201E-06   0.23387E+08 0.80714E+00 
c  TempK        0.10045E+05       4   0.48813E-05   0.50389E+01 0.81439E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3678e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.157           19.24     -0.00015879       -0.014148
v  Velocity[Y]             -15.465          15.367         0.29577         0.43349
v  Velocity[Z]             -25.323          11.907         -1.6374        -0.50796
v  ǁVelocityǁ         0.00016786          25.586           7.647          6.5228
v  Pressure                -566.35          196.38          20.825          26.076
v  k                    9.784e-011          9.2074         0.24446         0.53261
v  omega                    57.495     2.7318e+008     1.2912e+006           76851
v  TempK                    298.55          363.17          337.94          346.82
v  TurbVisc             2.452e-018       0.0019372     6.2623e-005      0.00022059
v  CourantNb            0.00018677          1.5704          0.7886         0.96971
v  FourierNb             0.0038111               1         0.42112         0.18919
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0045373     7.4196e-005      0.00020356

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0           2.927          0.6283         0.48328


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53443          2.1659          1.2097          1.1589


 INSTANT    0.870000000E-02   TIME STEP NUMBER             870
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925352E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10207E-01 0.46691E+01
   Friction velocity        uk    :  0.10207E-01 0.46652E+01
   Dimensionless distance   yplus :  0.69206E-02 0.29273E+01
   Friction thermal sca.    tstar :  0.12153E+01 0.25340E+03
   Rough dim-less th. sca.  tplus :  0.49026E-02 0.20737E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27043E+00      10   0.16251E-04   0.53912E+01 0.37196E+02 
c  Velocity[X]                                      0.22234E+01 
c  Velocity[Y]                                      0.14519E+01 
c  Velocity[Z]                                      0.17158E+01 
c  Pressure     0.18432E-04      20   0.33726E-03   0.18940E-01 0.45731E+02 
c  k            0.20440E-01      13   0.77394E-04   0.18018E+00 0.56329E+02 
c  omega        0.27922E+07       1   0.99978E-07   0.16233E+08 0.70329E+00 
c  TempK        0.10045E+05       4   0.48789E-05   0.50364E+01 0.81360E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3713e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.158          19.239     -0.00019274       -0.014148
v  Velocity[Y]             -15.332          15.363          0.2961         0.43426
v  Velocity[Z]             -25.317          11.904         -1.6374        -0.50794
v  ǁVelocityǁ         0.00016427          25.586          7.6466          6.5224
v  Pressure                -566.41          196.12          20.565          25.822
v  k                    9.783e-011          9.1934         0.24461         0.53284
v  omega                    57.495     2.7318e+008     1.2912e+006           76851
v  TempK                    298.55          363.17          337.94          346.83
v  TurbVisc            2.4517e-018       0.0019249     6.2668e-005      0.00022071
v  CourantNb            0.00015955          1.5695         0.78858         0.96971
v  FourierNb             0.0038108               1         0.42116         0.18926
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006        0.004461     7.4196e-005      0.00020355

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0          2.9273         0.62828         0.48326


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5613          2.1651          1.2097           1.159


 INSTANT    0.871000000E-02   TIME STEP NUMBER             871
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925286E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10051E-01 0.46692E+01
   Friction velocity        uk    :  0.10051E-01 0.46653E+01
   Dimensionless distance   yplus :  0.68149E-02 0.29277E+01
   Friction thermal sca.    tstar :  0.12151E+01 0.25733E+03
   Rough dim-less th. sca.  tplus :  0.48277E-02 0.20740E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27041E+00      10   0.16239E-04   0.54008E+01 0.37201E+02 
c  Velocity[X]                                      0.22251E+01 
c  Velocity[Y]                                      0.14579E+01 
c  Velocity[Z]                                      0.17178E+01 
c  Pressure     0.18763E-04      20   0.33558E-03   0.19282E-01 0.45366E+02 
c  k            0.20446E-01      13   0.76166E-04   0.17889E+00 0.56096E+02 
c  omega        0.27922E+07       1   0.98231E-07   0.10364E+08 0.60631E+00 
c  TempK        0.10045E+05       4   0.48771E-05   0.50366E+01 0.81311E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3745e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.159          19.238     -0.00022627       -0.014145
v  Velocity[Y]             -15.258          15.359         0.29642         0.43502
v  Velocity[Z]             -25.311            11.9         -1.6374         -0.5079
v  ǁVelocityǁ         0.00016086          25.585          7.6462          6.5221
v  Pressure                -566.46          195.86          20.307          25.569
v  k                    9.782e-011          9.1787         0.24475         0.53307
v  omega                    57.495     2.7318e+008     1.2912e+006           76851
v  TempK                    298.55          363.17          337.95          346.84
v  TurbVisc            2.4515e-018       0.0019112     6.2712e-005      0.00022082
v  CourantNb            0.00013877          1.5688         0.78857          0.9697
v  FourierNb             0.0038106               1         0.42121         0.18933
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0043736     7.4196e-005      0.00020354

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0          2.9277         0.62826         0.48324


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61025          2.1643          1.2098           1.159


 INSTANT    0.872000000E-02   TIME STEP NUMBER             872
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925289E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98679E-02 0.46694E+01
   Friction velocity        uk    :  0.98679E-02 0.46654E+01
   Dimensionless distance   yplus :  0.66906E-02 0.29280E+01
   Friction thermal sca.    tstar :  0.12151E+01 0.26212E+03
   Rough dim-less th. sca.  tplus :  0.47397E-02 0.20742E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27038E+00      10   0.16227E-04   0.54145E+01 0.37237E+02 
c  Velocity[X]                                      0.22280E+01 
c  Velocity[Y]                                      0.14666E+01 
c  Velocity[Z]                                      0.17199E+01 
c  Pressure     0.18906E-04      19   0.33732E-03   0.19432E-01 0.44931E+02 
c  k            0.20452E-01      12   0.75189E-04   0.17749E+00 0.55819E+02 
c  omega        0.27922E+07       1   0.98763E-07   0.10286E+08 0.61146E+00 
c  TempK        0.10045E+05       4   0.48755E-05   0.50363E+01 0.81265E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3771e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.159          19.237     -0.00025718       -0.014137
v  Velocity[Y]              -15.25          15.354         0.29675         0.43577
v  Velocity[Z]             -25.305          11.896         -1.6374        -0.50787
v  ǁVelocityǁ         0.00015801          25.584          7.6458          6.5218
v  Pressure                -566.49           195.6          20.053           25.32
v  k                   9.7811e-011          9.1636         0.24489         0.53329
v  omega                    57.495     2.7318e+008     1.2912e+006           76851
v  TempK                    298.55          363.17          337.95          346.85
v  TurbVisc            2.4512e-018       0.0018961     6.2756e-005      0.00022093
v  CourantNb            0.00013693          1.5681         0.78855          0.9697
v  FourierNb             0.0038104               1         0.42125          0.1894
v  total_pressure      1.0076e+005     1.0152e+005     1.0135e+005     1.0135e+005
v  Local Time Step          1e-006       0.0043097     7.4197e-005      0.00020352

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0           2.928         0.62824         0.48321


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62077          2.1637          1.2098          1.1591


 INSTANT    0.873000000E-02   TIME STEP NUMBER             873
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925300E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97143E-02 0.46695E+01
   Friction velocity        uk    :  0.97143E-02 0.46656E+01
   Dimensionless distance   yplus :  0.65865E-02 0.29284E+01
   Friction thermal sca.    tstar :  0.12150E+01 0.26626E+03
   Rough dim-less th. sca.  tplus :  0.46659E-02 0.20745E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27036E+00      10   0.16189E-04   0.54288E+01 0.37290E+02 
c  Velocity[X]                                      0.22314E+01 
c  Velocity[Y]                                      0.14749E+01 
c  Velocity[Z]                                      0.17226E+01 
c  Pressure     0.18867E-04      20   0.33692E-03   0.19393E-01 0.44678E+02 
c  k            0.20457E-01      12   0.74251E-04   0.17609E+00 0.55541E+02 
c  omega        0.27922E+07       1   0.10076E-06   0.13674E+08 0.67194E+00 
c  TempK        0.10045E+05       4   0.48742E-05   0.50385E+01 0.81225E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3794e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.16          19.236     -0.00028651       -0.014127
v  Velocity[Y]             -15.327           15.35         0.29708         0.43652
v  Velocity[Z]             -25.299          11.892         -1.6374        -0.50783
v  ǁVelocityǁ         0.00015606          25.584          7.6454          6.5215
v  Pressure                -566.51          195.34          19.801          25.073
v  k                   9.7801e-011          9.1479         0.24503         0.53351
v  omega                    57.496     2.7318e+008     1.2912e+006           76851
v  TempK                    298.55          363.17          337.96          346.85
v  TurbVisc             2.451e-018       0.0018807     6.2801e-005      0.00022104
v  CourantNb            0.00017465          1.5676         0.78853         0.96969
v  FourierNb             0.0038102               1          0.4213         0.18946
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006        0.004302     7.4197e-005      0.00020351

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0          2.9284         0.62822         0.48319


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41594          2.1632          1.2098          1.1592


 INSTANT    0.874000000E-02   TIME STEP NUMBER             874
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925365E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95391E-02 0.46696E+01
   Friction velocity        uk    :  0.95390E-02 0.46657E+01
   Dimensionless distance   yplus :  0.64676E-02 0.29287E+01
   Friction thermal sca.    tstar :  0.12149E+01 0.27116E+03
   Rough dim-less th. sca.  tplus :  0.45817E-02 0.20747E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27034E+00      10   0.16151E-04   0.54499E+01 0.37362E+02 
c  Velocity[X]                                      0.22380E+01 
c  Velocity[Y]                                      0.14855E+01 
c  Velocity[Z]                                      0.17264E+01 
c  Pressure     0.18879E-04      20   0.35269E-03   0.19407E-01 0.44105E+02 
c  k            0.20463E-01      12   0.73662E-04   0.17468E+00 0.55291E+02 
c  omega        0.27922E+07       1   0.10245E-06   0.17873E+08 0.73866E+00 
c  TempK        0.10045E+05       4   0.48731E-05   0.50440E+01 0.81211E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3815e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.16          19.235     -0.00031388       -0.014116
v  Velocity[Y]             -15.363          15.345         0.29741         0.43727
v  Velocity[Z]             -25.294          11.887         -1.6374         -0.5078
v  ǁVelocityǁ         0.00015541          25.583           7.645          6.5212
v  Pressure                 -566.5          195.08          19.553          24.828
v  k                   9.7792e-011          9.1315         0.24516         0.53372
v  omega                    57.496     2.7318e+008     1.2912e+006           76850
v  TempK                    298.55          363.17          337.96          346.86
v  TurbVisc            2.4508e-018        0.001867     6.2844e-005      0.00022115
v  CourantNb            0.00019039           1.567         0.78851         0.96969
v  FourierNb             0.0038099               1         0.42135         0.18953
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0043045     7.4198e-005       0.0002035

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0          2.9287         0.62821         0.48317


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61619          2.1627          1.2099          1.1592


 INSTANT    0.875000000E-02   TIME STEP NUMBER             875
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925309E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93880E-02 0.46698E+01
   Friction velocity        uk    :  0.93879E-02 0.46658E+01
   Dimensionless distance   yplus :  0.63652E-02 0.29290E+01
   Friction thermal sca.    tstar :  0.12148E+01 0.27553E+03
   Rough dim-less th. sca.  tplus :  0.45091E-02 0.20749E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27031E+00      10   0.16089E-04   0.54681E+01 0.37441E+02 
c  Velocity[X]                                      0.22428E+01 
c  Velocity[Y]                                      0.14972E+01 
c  Velocity[Z]                                      0.17282E+01 
c  Pressure     0.18652E-04      19   0.35610E-03   0.19176E-01 0.43744E+02 
c  k            0.20469E-01      12   0.72638E-04   0.17316E+00 0.55043E+02 
c  omega        0.27922E+07       1   0.10476E-06   0.24355E+08 0.83261E+00 
c  TempK        0.10045E+05       4   0.48726E-05   0.50495E+01 0.81179E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3845e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.16          19.233      -0.0003411       -0.014104
v  Velocity[Y]             -15.279           15.34         0.29776         0.43802
v  Velocity[Z]             -25.288          11.883         -1.6374        -0.50776
v  ǁVelocityǁ         0.00015655          25.583          7.6446          6.5209
v  Pressure                -566.49          194.83          19.307          24.587
v  k                   9.7782e-011          9.1147          0.2453         0.53393
v  omega                    57.496     2.7318e+008     1.2912e+006           76850
v  TempK                    298.55          363.17          337.97          346.87
v  TurbVisc            2.4505e-018        0.001857     6.2888e-005      0.00022126
v  CourantNb            0.00019683          1.5663         0.78849         0.96968
v  FourierNb             0.0038097               1         0.42139         0.18959
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0043333       7.42e-005      0.00020348

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0           2.929         0.62818         0.48314


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59405           2.162          1.2099          1.1593


 INSTANT    0.876000000E-02   TIME STEP NUMBER             876
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925406E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91909E-02 0.46699E+01
   Friction velocity        uk    :  0.91909E-02 0.46660E+01
   Dimensionless distance   yplus :  0.62316E-02 0.29293E+01
   Friction thermal sca.    tstar :  0.12149E+01 0.28144E+03
   Rough dim-less th. sca.  tplus :  0.44145E-02 0.20752E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27029E+00      10   0.16112E-04   0.54786E+01 0.37475E+02 
c  Velocity[X]                                      0.22488E+01 
c  Velocity[Y]                                      0.15018E+01 
c  Velocity[Z]                                      0.17281E+01 
c  Pressure     0.18501E-04      20   0.35640E-03   0.19024E-01 0.44785E+02 
c  k            0.20475E-01      12   0.71858E-04   0.17159E+00 0.54809E+02 
c  omega        0.27922E+07       1   0.10135E-06   0.14485E+08 0.68519E+00 
c  TempK        0.10046E+05       4   0.48726E-05   0.50580E+01 0.81169E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3875e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.161          19.232     -0.00036351       -0.014092
v  Velocity[Y]             -15.181          15.336          0.2981         0.43877
v  Velocity[Z]             -25.282          11.878         -1.6375        -0.50772
v  ǁVelocityǁ         0.00015993          25.582          7.6442          6.5206
v  Pressure                -566.48          194.57          19.054          24.339
v  k                   9.7773e-011          9.0972         0.24544         0.53413
v  omega                    57.496     2.7318e+008     1.2912e+006           76850
v  TempK                    298.55          363.17          337.97          346.88
v  TurbVisc            2.4503e-018        0.001846     6.2931e-005      0.00022137
v  CourantNb            0.00019709          1.5656         0.78847         0.96968
v  FourierNb             0.0038094               1         0.42144         0.18965
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0043136     7.4202e-005      0.00020347

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0          2.9293         0.62816         0.48312


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52827          2.1613          1.2099          1.1593


 INSTANT    0.877000000E-02   TIME STEP NUMBER             877
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925349E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89905E-02 0.46701E+01
   Friction velocity        uk    :  0.89905E-02 0.46661E+01
   Dimensionless distance   yplus :  0.60957E-02 0.29296E+01
   Friction thermal sca.    tstar :  0.12150E+01 0.28771E+03
   Rough dim-less th. sca.  tplus :  0.43182E-02 0.20754E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27027E+00      10   0.16193E-04   0.54910E+01 0.37514E+02 
c  Velocity[X]                                      0.22563E+01 
c  Velocity[Y]                                      0.15066E+01 
c  Velocity[Z]                                      0.17281E+01 
c  Pressure     0.18511E-04      19   0.36191E-03   0.19035E-01 0.44946E+02 
c  k            0.20480E-01      12   0.71109E-04   0.16983E+00 0.54586E+02 
c  omega        0.27922E+07       1   0.10126E-06   0.14718E+08 0.68349E+00 
c  TempK        0.10046E+05       4   0.48728E-05   0.50646E+01 0.81153E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3902e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.161           19.23     -0.00037971       -0.014079
v  Velocity[Y]             -15.132          15.331         0.29846         0.43951
v  Velocity[Z]             -25.276          11.873         -1.6375        -0.50769
v  ǁVelocityǁ           0.000166          25.582          7.6438          6.5204
v  Pressure                -566.47          194.31          18.801          24.091
v  k                   9.7764e-011          9.0792         0.24558         0.53434
v  omega                    57.496     2.7318e+008     1.2912e+006           76850
v  TempK                    298.55          363.17          337.98          346.89
v  TurbVisc              2.45e-018       0.0018409     6.2974e-005      0.00022147
v  CourantNb            0.00019736          1.5649         0.78846         0.96967
v  FourierNb             0.0038091               1         0.42149         0.18971
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0042803     7.4203e-005      0.00020346

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.51          306.59
v  Yplus               0          2.9296         0.62813         0.48309


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55234          2.1607          1.2099          1.1594


 INSTANT    0.878000000E-02   TIME STEP NUMBER             878
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925329E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88422E-02 0.46702E+01
   Friction velocity        uk    :  0.88422E-02 0.46663E+01
   Dimensionless distance   yplus :  0.59952E-02 0.29300E+01
   Friction thermal sca.    tstar :  0.12148E+01 0.29254E+03
   Rough dim-less th. sca.  tplus :  0.42470E-02 0.20756E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27025E+00      10   0.16120E-04   0.55007E+01 0.37542E+02 
c  Velocity[X]                                      0.22637E+01 
c  Velocity[Y]                                      0.15097E+01 
c  Velocity[Z]                                      0.17272E+01 
c  Pressure     0.18427E-04      19   0.35654E-03   0.18951E-01 0.44464E+02 
c  k            0.20486E-01      12   0.70295E-04   0.16792E+00 0.54350E+02 
c  omega        0.27922E+07       1   0.10015E-06   0.12069E+08 0.63431E+00 
c  TempK        0.10046E+05       4   0.48737E-05   0.50725E+01 0.81158E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3925e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.161          19.228      -0.0003896       -0.014062
v  Velocity[Y]             -15.164          15.327         0.29882         0.44026
v  Velocity[Z]             -25.271          11.868         -1.6375        -0.50766
v  ǁVelocityǁ         0.00017534          25.582          7.6434          6.5201
v  Pressure                -566.44          194.06          18.551          23.845
v  k                   9.7755e-011          9.0607         0.24572         0.53454
v  omega                    57.496     2.7318e+008     1.2912e+006           76850
v  TempK                    298.56          363.17          337.98           346.9
v  TurbVisc            2.4498e-018       0.0018418     6.3017e-005      0.00022158
v  CourantNb             0.0001873          1.5643         0.78844         0.96966
v  FourierNb             0.0038088               1         0.42153         0.18977
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0042463     7.4204e-005      0.00020344

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0            2.93         0.62811         0.48307


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61311          2.1602            1.21          1.1594


 INSTANT    0.879000000E-02   TIME STEP NUMBER             879
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925337E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.86792E-02 0.46704E+01
   Friction velocity        uk    :  0.86792E-02 0.46665E+01
   Dimensionless distance   yplus :  0.58846E-02 0.29303E+01
   Friction thermal sca.    tstar :  0.12147E+01 0.29804E+03
   Rough dim-less th. sca.  tplus :  0.41687E-02 0.20758E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27022E+00      10   0.15935E-04   0.55189E+01 0.37620E+02 
c  Velocity[X]                                      0.22732E+01 
c  Velocity[Y]                                      0.15158E+01 
c  Velocity[Z]                                      0.17300E+01 
c  Pressure     0.18352E-04      20   0.36005E-03   0.18875E-01 0.43610E+02 
c  k            0.20492E-01      12   0.69677E-04   0.16611E+00 0.54142E+02 
c  omega        0.27922E+07       1   0.10216E-06   0.17216E+08 0.71639E+00 
c  TempK        0.10046E+05       4   0.48744E-05   0.50840E+01 0.81197E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3945e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.161          19.227     -0.00039531       -0.014044
v  Velocity[Y]             -15.222          15.322         0.29918           0.441
v  Velocity[Z]             -25.265          11.863         -1.6376        -0.50763
v  ǁVelocityǁ         0.00018719          25.581           7.643          6.5198
v  Pressure                -566.38           193.8          18.306          23.604
v  k                   9.7746e-011          9.0417         0.24585         0.53475
v  omega                    57.496     2.7318e+008     1.2912e+006           76850
v  TempK                    298.56          363.17          337.99          346.91
v  TurbVisc            2.4496e-018       0.0018425      6.306e-005      0.00022168
v  CourantNb            0.00012897          1.5638         0.78842         0.96966
v  FourierNb             0.0038085               1         0.42158         0.18983
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0042155     7.4206e-005      0.00020342

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9303         0.62808         0.48305


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58005          2.1597            1.21          1.1595


 INSTANT    0.880000000E-02   TIME STEP NUMBER             880
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925342E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84977E-02 0.46706E+01
   Friction velocity        uk    :  0.84977E-02 0.46666E+01
   Dimensionless distance   yplus :  0.57616E-02 0.29306E+01
   Friction thermal sca.    tstar :  0.12146E+01 0.30441E+03
   Rough dim-less th. sca.  tplus :  0.40816E-02 0.20760E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27020E+00      10   0.15885E-04   0.55361E+01 0.37697E+02 
c  Velocity[X]                                      0.22829E+01 
c  Velocity[Y]                                      0.15236E+01 
c  Velocity[Z]                                      0.17296E+01 
c  Pressure     0.18477E-04      20   0.35009E-03   0.19003E-01 0.43887E+02 
c  k            0.20498E-01      12   0.68940E-04   0.16440E+00 0.53945E+02 
c  omega        0.27922E+07       1   0.10267E-06   0.20048E+08 0.75970E+00 
c  TempK        0.10046E+05       4   0.48745E-05   0.50967E+01 0.81232E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3973e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.161          19.225     -0.00039619       -0.014025
v  Velocity[Y]             -15.179          15.317         0.29954         0.44173
v  Velocity[Z]             -25.259          11.857         -1.6376        -0.50759
v  ǁVelocityǁ         0.00020109          25.581          7.6426          6.5196
v  Pressure                -566.33          193.54           18.06          23.362
v  k                   9.7737e-011          9.0222         0.24599         0.53496
v  omega                    57.496     2.7318e+008     1.2912e+006           76850
v  TempK                    298.56          363.17          337.99          346.92
v  TurbVisc            2.4494e-018        0.001843     6.3103e-005      0.00022178
v  CourantNb           8.5444e-005          1.5631          0.7884         0.96965
v  FourierNb             0.0038082               1         0.42163         0.18988
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0041857      7.421e-005      0.00020341

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9306         0.62806         0.48302


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44916          2.1591            1.21          1.1595


 INSTANT    0.881000000E-02   TIME STEP NUMBER             881
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925263E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83368E-02 0.46708E+01
   Friction velocity        uk    :  0.83367E-02 0.46668E+01
   Dimensionless distance   yplus :  0.56525E-02 0.29309E+01
   Friction thermal sca.    tstar :  0.12145E+01 0.31029E+03
   Rough dim-less th. sca.  tplus :  0.40042E-02 0.20763E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27018E+00      10   0.15917E-04   0.55437E+01 0.37725E+02 
c  Velocity[X]                                      0.22892E+01 
c  Velocity[Y]                                      0.15252E+01 
c  Velocity[Z]                                      0.17293E+01 
c  Pressure     0.18726E-04      20   0.35417E-03   0.19258E-01 0.44324E+02 
c  k            0.20505E-01      12   0.68502E-04   0.16290E+00 0.53787E+02 
c  omega        0.27922E+07       1   0.10230E-06   0.18450E+08 0.73410E+00 
c  TempK        0.10046E+05       4   0.48748E-05   0.51143E+01 0.81286E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4004e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.161          19.223     -0.00039315       -0.014008
v  Velocity[Y]             -15.072          15.312         0.29992         0.44246
v  Velocity[Z]             -25.254          11.852         -1.6376        -0.50755
v  ǁVelocityǁ         0.00021784          25.581          7.6422          6.5194
v  Pressure                -566.29          193.29          17.811          23.118
v  k                   9.7728e-011          9.0021         0.24613         0.53517
v  omega                    57.496     2.7318e+008     1.2912e+006           76849
v  TempK                    298.56          363.17             338          346.93
v  TurbVisc            2.4491e-018       0.0018434     6.3147e-005      0.00022188
v  CourantNb           7.5814e-005          1.5624         0.78838         0.96964
v  FourierNb             0.0038079               1         0.42168         0.18994
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0041471     7.4213e-005       0.0002034

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9309         0.62803           0.483


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39054          2.1584          1.2101          1.1596


 INSTANT    0.882000000E-02   TIME STEP NUMBER             882
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925346E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81786E-02 0.46709E+01
   Friction velocity        uk    :  0.81785E-02 0.46670E+01
   Dimensionless distance   yplus :  0.55452E-02 0.29312E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.31629E+03
   Rough dim-less th. sca.  tplus :  0.39283E-02 0.20765E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27015E+00      10   0.15886E-04   0.55582E+01 0.37790E+02 
c  Velocity[X]                                      0.23022E+01 
c  Velocity[Y]                                      0.15279E+01 
c  Velocity[Z]                                      0.17281E+01 
c  Pressure     0.18888E-04      21   0.36328E-03   0.19424E-01 0.44115E+02 
c  k            0.20511E-01      12   0.67927E-04   0.16147E+00 0.53665E+02 
c  omega        0.27922E+07       1   0.10059E-06   0.12332E+08 0.63427E+00 
c  TempK        0.10046E+05       4   0.48756E-05   0.51320E+01 0.81365E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4032e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.161          19.221     -0.00038563        -0.01399
v  Velocity[Y]             -15.004          15.308          0.3003         0.44319
v  Velocity[Z]             -25.248          11.853         -1.6376        -0.50752
v  ǁVelocityǁ         0.00023711          25.581          7.6418          6.5191
v  Pressure                -566.24          193.03          17.564          22.876
v  k                    9.772e-011          8.9817         0.24627         0.53538
v  omega                    57.496     2.7318e+008     1.2912e+006           76849
v  TempK                    298.56          363.17             338          346.93
v  TurbVisc            2.4489e-018       0.0018436     6.3191e-005      0.00022199
v  CourantNb            0.00012204          1.5617         0.78836         0.96964
v  FourierNb             0.0038076               1         0.42173            0.19
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0041048     7.4216e-005      0.00020338

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9312         0.62801         0.48298


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53672          2.1578          1.2101          1.1596


 INSTANT    0.883000000E-02   TIME STEP NUMBER             883
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925362E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.79888E-02 0.46711E+01
   Friction velocity        uk    :  0.79888E-02 0.46672E+01
   Dimensionless distance   yplus :  0.54165E-02 0.29315E+01
   Friction thermal sca.    tstar :  0.12145E+01 0.32381E+03
   Rough dim-less th. sca.  tplus :  0.38371E-02 0.20767E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27013E+00      10   0.15816E-04   0.55767E+01 0.37893E+02 
c  Velocity[X]                                      0.23167E+01 
c  Velocity[Y]                                      0.15331E+01 
c  Velocity[Z]                                      0.17269E+01 
c  Pressure     0.19066E-04      19   0.36002E-03   0.19605E-01 0.43919E+02 
c  k            0.20518E-01      12   0.67539E-04   0.16004E+00 0.53543E+02 
c  omega        0.27922E+07       1   0.10121E-06   0.13869E+08 0.66323E+00 
c  TempK        0.10046E+05       4   0.48745E-05   0.51518E+01 0.81455E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4055e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.161          19.219     -0.00037316       -0.013964
v  Velocity[Y]              -15.01          15.303          0.3007         0.44392
v  Velocity[Z]             -25.243          11.855         -1.6377        -0.50748
v  ǁVelocityǁ         0.00025914          25.581          7.6414          6.5189
v  Pressure                -566.17          192.77          17.318          22.634
v  k                   9.7711e-011          8.9607         0.24641         0.53559
v  omega                    57.496     2.7318e+008     1.2912e+006           76849
v  TempK                    298.57          363.17          338.01          346.94
v  TurbVisc            2.4487e-018       0.0018439     6.3236e-005      0.00022209
v  CourantNb            0.00019917          1.5612         0.78835         0.96963
v  FourierNb             0.0038072               1         0.42178         0.19005
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040653     7.4218e-005      0.00020337

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9315         0.62799         0.48296


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56468          2.1572          1.2101          1.1597


 INSTANT    0.884000000E-02   TIME STEP NUMBER             884
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925357E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77556E-02 0.46713E+01
   Friction velocity        uk    :  0.77555E-02 0.46674E+01
   Dimensionless distance   yplus :  0.52584E-02 0.29318E+01
   Friction thermal sca.    tstar :  0.12146E+01 0.33355E+03
   Rough dim-less th. sca.  tplus :  0.37251E-02 0.20769E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27010E+00      10   0.15917E-04   0.55999E+01 0.37980E+02 
c  Velocity[X]                                      0.23356E+01 
c  Velocity[Y]                                      0.15354E+01 
c  Velocity[Z]                                      0.17288E+01 
c  Pressure     0.19342E-04      19   0.37077E-03   0.19886E-01 0.44658E+02 
c  k            0.20525E-01      12   0.67085E-04   0.15860E+00 0.53415E+02 
c  omega        0.27922E+07       1   0.10327E-06   0.18262E+08 0.73575E+00 
c  TempK        0.10046E+05       4   0.48738E-05   0.51692E+01 0.81551E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4075e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.16          19.217     -0.00035935       -0.013938
v  Velocity[Y]             -15.097          15.298          0.3011         0.44463
v  Velocity[Z]             -25.237          11.856         -1.6377        -0.50744
v  ǁVelocityǁ         0.00028385          25.581           7.641          6.5186
v  Pressure                -566.09           192.5          17.068          22.388
v  k                   9.7703e-011          9.0152         0.24655         0.53581
v  omega                    57.497     2.7318e+008     1.2912e+006           76849
v  TempK                    298.57          363.17          338.01          346.95
v  TurbVisc            2.4485e-018        0.001844     6.3281e-005      0.00022219
v  CourantNb            0.00019957          1.5607         0.78833         0.96962
v  FourierNb             0.0038069               1         0.42183         0.19011
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040608     7.4221e-005      0.00020335

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9318         0.62797         0.48294


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41656          2.1568          1.2102          1.1597


 INSTANT    0.885000000E-02   TIME STEP NUMBER             885
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925315E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76241E-02 0.46716E+01
   Friction velocity        uk    :  0.76241E-02 0.46676E+01
   Dimensionless distance   yplus :  0.51693E-02 0.29321E+01
   Friction thermal sca.    tstar :  0.12144E+01 0.33930E+03
   Rough dim-less th. sca.  tplus :  0.36620E-02 0.20771E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27008E+00      10   0.15805E-04   0.56253E+01 0.38078E+02 
c  Velocity[X]                                      0.23530E+01 
c  Velocity[Y]                                      0.15399E+01 
c  Velocity[Z]                                      0.17325E+01 
c  Pressure     0.19687E-04      19   0.37692E-03   0.20239E-01 0.43534E+02 
c  k            0.20532E-01      12   0.66438E-04   0.15762E+00 0.53370E+02 
c  omega        0.27922E+07       1   0.10390E-06   0.18807E+08 0.74617E+00 
c  TempK        0.10046E+05       4   0.48725E-05   0.51901E+01 0.81689E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4095e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.16          19.215     -0.00034428       -0.013909
v  Velocity[Y]             -15.146          15.293          0.3015         0.44535
v  Velocity[Z]             -25.231          11.856         -1.6377        -0.50739
v  ǁVelocityǁ         0.00031073          25.581          7.6406          6.5184
v  Pressure                -565.98          192.25          16.826           22.15
v  k                   9.7695e-011          8.9612         0.24669         0.53603
v  omega                    57.497     2.7318e+008     1.2912e+006           76849
v  TempK                    298.57          363.17          338.02          346.96
v  TurbVisc            2.4483e-018       0.0018442     6.3326e-005       0.0002223
v  CourantNb            0.00019998          1.5602         0.78831         0.96961
v  FourierNb             0.0038066               1         0.42188         0.19016
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040628     7.4223e-005      0.00020333

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9321         0.62795         0.48292


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51219          2.1564          1.2102          1.1598


 INSTANT    0.886000000E-02   TIME STEP NUMBER             886
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925364E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.74431E-02 0.46718E+01
   Friction velocity        uk    :  0.74431E-02 0.46678E+01
   Dimensionless distance   yplus :  0.50465E-02 0.29323E+01
   Friction thermal sca.    tstar :  0.12143E+01 0.34756E+03
   Rough dim-less th. sca.  tplus :  0.35750E-02 0.20773E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27006E+00      10   0.15762E-04   0.56531E+01 0.38206E+02 
c  Velocity[X]                                      0.23730E+01 
c  Velocity[Y]                                      0.15461E+01 
c  Velocity[Z]                                      0.17341E+01 
c  Pressure     0.19474E-04      19   0.36254E-03   0.20016E-01 0.43790E+02 
c  k            0.20540E-01      12   0.66024E-04   0.15658E+00 0.53320E+02 
c  omega        0.27922E+07       1   0.10455E-06   0.20179E+08 0.77049E+00 
c  TempK        0.10046E+05       4   0.48707E-05   0.52002E+01 0.81790E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4122e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.16          19.212     -0.00032863       -0.013879
v  Velocity[Y]             -15.071          15.288         0.30192         0.44606
v  Velocity[Z]             -25.226          11.855         -1.6377        -0.50734
v  ǁVelocityǁ         0.00033258          25.581          7.6402          6.5182
v  Pressure                -565.88          191.99          16.581           21.91
v  k                   9.7687e-011          8.8954         0.24683         0.53625
v  omega                    57.497     2.7318e+008     1.2912e+006           76849
v  TempK                    298.58          363.17          338.02          346.97
v  TurbVisc            2.4481e-018       0.0018443     6.3371e-005      0.00022241
v  CourantNb            0.00020037          1.5595         0.78829          0.9696
v  FourierNb             0.0038063               1         0.42193         0.19021
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040681     7.4225e-005      0.00020331

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9323         0.62793          0.4829


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56127          2.1558          1.2102          1.1598


 INSTANT    0.887000000E-02   TIME STEP NUMBER             887
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925338E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72504E-02 0.46720E+01
   Friction velocity        uk    :  0.72504E-02 0.46680E+01
   Dimensionless distance   yplus :  0.49159E-02 0.29326E+01
   Friction thermal sca.    tstar :  0.12142E+01 0.35680E+03
   Rough dim-less th. sca.  tplus :  0.34824E-02 0.20775E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27003E+00      10   0.15680E-04   0.56676E+01 0.38265E+02 
c  Velocity[X]                                      0.23899E+01 
c  Velocity[Y]                                      0.15427E+01 
c  Velocity[Z]                                      0.17349E+01 
c  Pressure     0.19345E-04      19   0.35491E-03   0.19880E-01 0.43834E+02 
c  k            0.20548E-01      12   0.65799E-04   0.15562E+00 0.53298E+02 
c  omega        0.27922E+07       1   0.10185E-06   0.11238E+08 0.63122E+00 
c  TempK        0.10046E+05       4   0.48681E-05   0.52015E+01 0.81854E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4149e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.159           19.21     -0.00031235       -0.013847
v  Velocity[Y]              -14.99          15.284         0.30234         0.44678
v  Velocity[Z]              -25.22          11.853         -1.6377        -0.50729
v  ǁVelocityǁ          0.0003324          25.581          7.6398          6.5179
v  Pressure                -565.75          191.73          16.336           21.67
v  k                    9.768e-011          9.0086         0.24697         0.53648
v  omega                    57.497     2.7318e+008     1.2912e+006           76849
v  TempK                    298.58          363.17          338.03          346.98
v  TurbVisc            2.4479e-018       0.0018445     6.3416e-005      0.00022252
v  CourantNb            0.00020078          1.5589         0.78827         0.96958
v  FourierNb             0.0038061               1         0.42197         0.19026
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040591     7.4228e-005      0.00020329

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9326         0.62791         0.48288


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.37469          2.1552          1.2102          1.1598


 INSTANT    0.888000000E-02   TIME STEP NUMBER             888
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925300E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70717E-02 0.46722E+01
   Friction velocity        uk    :  0.70717E-02 0.46683E+01
   Dimensionless distance   yplus :  0.47947E-02 0.29329E+01
   Friction thermal sca.    tstar :  0.12141E+01 0.36582E+03
   Rough dim-less th. sca.  tplus :  0.33966E-02 0.20777E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.27001E+00      10   0.15722E-04   0.56904E+01 0.38354E+02 
c  Velocity[X]                                      0.24082E+01 
c  Velocity[Y]                                      0.15433E+01 
c  Velocity[Z]                                      0.17390E+01 
c  Pressure     0.19358E-04      19   0.35171E-03   0.19889E-01 0.43562E+02 
c  k            0.20556E-01      12   0.65685E-04   0.15480E+00 0.53300E+02 
c  omega        0.27922E+07       1   0.10228E-06   0.11277E+08 0.63763E+00 
c  TempK        0.10046E+05       4   0.48654E-05   0.52037E+01 0.81899E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4175e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.159          19.208     -0.00029109       -0.013812
v  Velocity[Y]             -14.958          15.279         0.30278         0.44749
v  Velocity[Z]             -25.215          11.852         -1.6377        -0.50724
v  ǁVelocityǁ         0.00033264          25.582          7.6394          6.5177
v  Pressure                -565.61          191.47          16.094          21.432
v  k                   9.7672e-011          9.1683         0.24711         0.53671
v  omega                    57.497     2.7318e+008     1.2912e+006           76848
v  TempK                    298.59          363.17          338.03          346.99
v  TurbVisc            2.4477e-018       0.0018447     6.3461e-005      0.00022264
v  CourantNb            0.00017965          1.5582         0.78825         0.96957
v  FourierNb             0.0038058               1         0.42202         0.19032
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040484     7.4232e-005      0.00020328

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9329         0.62789         0.48287


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54741          2.1546          1.2103          1.1599


 INSTANT    0.889000000E-02   TIME STEP NUMBER             889
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925352E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69151E-02 0.46724E+01
   Friction velocity        uk    :  0.69151E-02 0.46685E+01
   Dimensionless distance   yplus :  0.46885E-02 0.29332E+01
   Friction thermal sca.    tstar :  0.12140E+01 0.37411E+03
   Rough dim-less th. sca.  tplus :  0.33214E-02 0.20779E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26998E+00      10   0.15737E-04   0.57137E+01 0.38462E+02 
c  Velocity[X]                                      0.24292E+01 
c  Velocity[Y]                                      0.15435E+01 
c  Velocity[Z]                                      0.17410E+01 
c  Pressure     0.19600E-04      19   0.37226E-03   0.20133E-01 0.43613E+02 
c  k            0.20564E-01      12   0.65480E-04   0.15414E+00 0.53320E+02 
c  omega        0.27922E+07       1   0.10463E-06   0.15606E+08 0.71426E+00 
c  TempK        0.10046E+05       4   0.48629E-05   0.52117E+01 0.81966E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4196e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.158          19.206     -0.00026835       -0.013774
v  Velocity[Y]             -15.022          15.274         0.30322          0.4482
v  Velocity[Z]              -25.21          11.854         -1.6377        -0.50719
v  ǁVelocityǁ         0.00033352          25.582           7.639          6.5175
v  Pressure                -565.45          191.21          15.853          21.195
v  k                   9.7665e-011          9.2607         0.24725         0.53695
v  omega                    57.497     2.7318e+008     1.2912e+006           76848
v  TempK                    298.59          363.17          338.04             347
v  TurbVisc            2.4475e-018        0.001845     6.3507e-005      0.00022276
v  CourantNb            0.00019705          1.5577         0.78824         0.96956
v  FourierNb             0.0038055               1         0.42207         0.19038
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040736     7.4236e-005      0.00020326

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9332         0.62787         0.48285


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5294          2.1542          1.2103          1.1599


 INSTANT    0.890000000E-02   TIME STEP NUMBER             890
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925340E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66789E-02 0.46727E+01
   Friction velocity        uk    :  0.66789E-02 0.46687E+01
   Dimensionless distance   yplus :  0.45284E-02 0.29334E+01
   Friction thermal sca.    tstar :  0.12141E+01 0.38734E+03
   Rough dim-less th. sca.  tplus :  0.32079E-02 0.20781E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26996E+00      10   0.15817E-04   0.57403E+01 0.38598E+02 
c  Velocity[X]                                      0.24488E+01 
c  Velocity[Y]                                      0.15509E+01 
c  Velocity[Z]                                      0.17405E+01 
c  Pressure     0.19741E-04      19   0.36332E-03   0.20276E-01 0.42929E+02 
c  k            0.20572E-01      12   0.65266E-04   0.15351E+00 0.53363E+02 
c  omega        0.27922E+07       1   0.10760E-06   0.22760E+08 0.82386E+00 
c  TempK        0.10046E+05       4   0.48610E-05   0.52179E+01 0.82038E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4215e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.158          19.203     -0.00023901       -0.013734
v  Velocity[Y]             -15.063          15.269         0.30366         0.44891
v  Velocity[Z]             -25.204          11.855         -1.6378        -0.50714
v  ǁVelocityǁ         0.00033499          25.582          7.6386          6.5172
v  Pressure                -565.27          190.96          15.617          20.963
v  k                   9.7658e-011           9.192         0.24739         0.53719
v  omega                    57.497     2.7318e+008     1.2912e+006           76848
v  TempK                    298.59          363.17          338.04             347
v  TurbVisc            2.4473e-018       0.0018453     6.3553e-005      0.00022288
v  CourantNb            0.00019409          1.5573         0.78822         0.96955
v  FourierNb             0.0038053               1         0.42212         0.19044
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0041102      7.424e-005      0.00020325

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9334         0.62785         0.48284


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48283          2.1538          1.2103            1.16


 INSTANT    0.891000000E-02   TIME STEP NUMBER             891
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925323E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64438E-02 0.46729E+01
   Friction velocity        uk    :  0.64437E-02 0.46690E+01
   Dimensionless distance   yplus :  0.43690E-02 0.29337E+01
   Friction thermal sca.    tstar :  0.12141E+01 0.40148E+03
   Rough dim-less th. sca.  tplus :  0.30950E-02 0.20783E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26993E+00      10   0.15753E-04   0.57500E+01 0.38675E+02 
c  Velocity[X]                                      0.24702E+01 
c  Velocity[Y]                                      0.15515E+01 
c  Velocity[Z]                                      0.17283E+01 
c  Pressure     0.19607E-04      19   0.36166E-03   0.20136E-01 0.44689E+02 
c  k            0.20581E-01      12   0.65189E-04   0.15313E+00 0.53407E+02 
c  omega        0.27922E+07       1   0.10891E-06   0.24404E+08 0.85802E+00 
c  TempK        0.10046E+05       4   0.48600E-05   0.52252E+01 0.82092E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4243e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.157          19.201     -0.00020714       -0.013693
v  Velocity[Y]             -15.009          15.264         0.30412         0.44961
v  Velocity[Z]             -25.198          11.855         -1.6377         -0.5071
v  ǁVelocityǁ         0.00033689          25.582          7.6383           6.517
v  Pressure                -565.08          190.69          15.368          20.718
v  k                   9.7651e-011          9.2315         0.24753         0.53743
v  omega                    57.497     2.7318e+008     1.2912e+006           76848
v  TempK                    298.59          363.17          338.05          347.01
v  TurbVisc            2.4472e-018       0.0018456     6.3599e-005        0.000223
v  CourantNb             0.0001732          1.5566          0.7882         0.96955
v  FourierNb              0.003805               1         0.42217          0.1905
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0041093     7.4245e-005      0.00020324

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9337         0.62783         0.48282


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52478          2.1532          1.2104            1.16


 INSTANT    0.892000000E-02   TIME STEP NUMBER             892
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925316E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62211E-02 0.46732E+01
   Friction velocity        uk    :  0.62211E-02 0.46692E+01
   Dimensionless distance   yplus :  0.42180E-02 0.29339E+01
   Friction thermal sca.    tstar :  0.12140E+01 0.41585E+03
   Rough dim-less th. sca.  tplus :  0.29881E-02 0.20784E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26991E+00      10   0.15761E-04   0.57632E+01 0.38710E+02 
c  Velocity[X]                                      0.24912E+01 
c  Velocity[Y]                                      0.15475E+01 
c  Velocity[Z]                                      0.17246E+01 
c  Pressure     0.19637E-04      19   0.36407E-03   0.20163E-01 0.45698E+02 
c  k            0.20590E-01      12   0.66005E-04   0.15275E+00 0.53442E+02 
c  omega        0.27922E+07       1   0.10567E-06   0.12683E+08 0.69960E+00 
c  TempK        0.10046E+05       4   0.48589E-05   0.52333E+01 0.82161E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4272e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.156          19.198     -0.00017176       -0.013649
v  Velocity[Y]             -14.954           15.26         0.30458         0.45032
v  Velocity[Z]             -25.193          11.855         -1.6377        -0.50707
v  ǁVelocityǁ         0.00033981          25.583          7.6379          6.5167
v  Pressure                -564.89          190.42          15.112          20.468
v  k                   9.7644e-011          9.4028         0.24767         0.53768
v  omega                    57.497     2.7318e+008     1.2912e+006           76848
v  TempK                    298.59          363.17          338.05          347.02
v  TurbVisc             2.447e-018       0.0018461     6.3646e-005      0.00022313
v  CourantNb            0.00014725          1.5559         0.78818         0.96954
v  FourierNb             0.0038047               1         0.42222         0.19056
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040916     7.4249e-005      0.00020322

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9339         0.62781         0.48281


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47535          2.1525          1.2104          1.1601


 INSTANT    0.893000000E-02   TIME STEP NUMBER             893
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925297E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60384E-02 0.46734E+01
   Friction velocity        uk    :  0.60384E-02 0.46695E+01
   Dimensionless distance   yplus :  0.40942E-02 0.29342E+01
   Friction thermal sca.    tstar :  0.12138E+01 0.42844E+03
   Rough dim-less th. sca.  tplus :  0.29003E-02 0.20786E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26988E+00      10   0.15696E-04   0.57822E+01 0.38798E+02 
c  Velocity[X]                                      0.25112E+01 
c  Velocity[Y]                                      0.15472E+01 
c  Velocity[Z]                                      0.17238E+01 
c  Pressure     0.19785E-04      19   0.37863E-03   0.20313E-01 0.45842E+02 
c  k            0.20599E-01      12   0.66202E-04   0.15246E+00 0.53475E+02 
c  omega        0.27922E+07       1   0.10601E-06   0.12182E+08 0.70027E+00 
c  TempK        0.10046E+05       4   0.48574E-05   0.52430E+01 0.82240E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step       6.43e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.156          19.197     -0.00013935       -0.013605
v  Velocity[Y]              -14.94          15.255         0.30505         0.45102
v  Velocity[Z]             -25.187          11.855         -1.6377        -0.50703
v  ǁVelocityǁ         0.00034325          25.583          7.6375          6.5165
v  Pressure                 -564.7          190.15          14.856          20.216
v  k                   9.7637e-011          9.5046         0.24782         0.53793
v  omega                    57.497     2.7318e+008     1.2912e+006           76848
v  TempK                    298.59          363.17          338.06          347.03
v  TurbVisc            2.4468e-018       0.0018466     6.3692e-005      0.00022326
v  CourantNb            0.00012012          1.5552         0.78817         0.96953
v  FourierNb             0.0038045               1         0.42227         0.19062
v  total_pressure      1.0076e+005     1.0152e+005     1.0134e+005     1.0135e+005
v  Local Time Step          1e-006       0.0040758     7.4253e-005      0.00020321

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9342         0.62779          0.4828


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41649          2.1519          1.2104          1.1602


 INSTANT    0.894000000E-02   TIME STEP NUMBER             894
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925308E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57910E-02 0.46737E+01
   Friction velocity        uk    :  0.57910E-02 0.46697E+01
   Dimensionless distance   yplus :  0.39264E-02 0.29344E+01
   Friction thermal sca.    tstar :  0.12138E+01 0.44675E+03
   Rough dim-less th. sca.  tplus :  0.27815E-02 0.20788E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26985E+00      10   0.15800E-04   0.58036E+01 0.38894E+02 
c  Velocity[X]                                      0.25324E+01 
c  Velocity[Y]                                      0.15472E+01 
c  Velocity[Z]                                      0.17240E+01 
c  Pressure     0.19777E-04      19   0.37070E-03   0.20302E-01 0.46165E+02 
c  k            0.20607E-01      12   0.66103E-04   0.15209E+00 0.53491E+02 
c  omega        0.27922E+07       1   0.10648E-06   0.13356E+08 0.71861E+00 
c  TempK        0.10046E+05       4   0.48560E-05   0.52586E+01 0.82350E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4324e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.157          19.195     -0.00011156       -0.013566
v  Velocity[Y]             -14.999           15.25         0.30553         0.45173
v  Velocity[Z]             -25.182          11.854         -1.6377        -0.50699
v  ǁVelocityǁ         0.00034752          25.583          7.6371          6.5162
v  Pressure                -564.51          189.87          14.599          19.964
v  k                   9.7631e-011          9.5647         0.24796         0.53819
v  omega                    57.497     2.7318e+008     1.2912e+006           76848
v  TempK                     298.6          363.17          338.06          347.04
v  TurbVisc            2.4466e-018       0.0018473     6.3739e-005      0.00022339
v  CourantNb           9.2164e-005          1.5546         0.78815         0.96952
v  FourierNb             0.0038042               1         0.42231         0.19069
v  total_pressure      1.0076e+005     1.0151e+005     1.0134e+005     1.0134e+005
v  Local Time Step          1e-006       0.0040634     7.4258e-005       0.0002032

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9344         0.62777         0.48279


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47824          2.1514          1.2105          1.1602


 INSTANT    0.895000000E-02   TIME STEP NUMBER             895
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925309E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.55539E-02 0.46739E+01
   Friction velocity        uk    :  0.55539E-02 0.46700E+01
   Dimensionless distance   yplus :  0.37656E-02 0.29347E+01
   Friction thermal sca.    tstar :  0.12138E+01 0.46582E+03
   Rough dim-less th. sca.  tplus :  0.26676E-02 0.20789E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26983E+00      10   0.15735E-04   0.58313E+01 0.39014E+02 
c  Velocity[X]                                      0.25542E+01 
c  Velocity[Y]                                      0.15494E+01 
c  Velocity[Z]                                      0.17277E+01 
c  Pressure     0.19718E-04      19   0.36726E-03   0.20239E-01 0.45574E+02 
c  k            0.20616E-01      12   0.65854E-04   0.15201E+00 0.53547E+02 
c  omega        0.27922E+07       1   0.10890E-06   0.20118E+08 0.80989E+00 
c  TempK        0.10046E+05       4   0.48552E-05   0.52773E+01 0.82488E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4345e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.159          19.194    -8.8039e-005       -0.013527
v  Velocity[Y]             -15.078          15.245         0.30601         0.45243
v  Velocity[Z]             -25.177          11.853         -1.6377        -0.50696
v  ǁVelocityǁ         0.00035241          25.584          7.6368           6.516
v  Pressure                -564.31          189.61          14.346          19.715
v  k                   9.7624e-011          9.4901          0.2481         0.53846
v  omega                    57.498     2.7318e+008     1.2912e+006           76848
v  TempK                     298.6          363.17          338.07          347.05
v  TurbVisc            2.4465e-018        0.001848     6.3785e-005      0.00022352
v  CourantNb            6.968e-005          1.5541         0.78813         0.96951
v  FourierNb              0.003804               1         0.42236         0.19075
v  total_pressure      1.0076e+005     1.0151e+005     1.0134e+005     1.0134e+005
v  Local Time Step          1e-006       0.0040038     7.4262e-005      0.00020319

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9347         0.62775         0.48278


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4406           2.151          1.2105          1.1603


 INSTANT    0.896000000E-02   TIME STEP NUMBER             896
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925427E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53145E-02 0.46742E+01
   Friction velocity        uk    :  0.53145E-02 0.46703E+01
   Dimensionless distance   yplus :  0.36033E-02 0.29349E+01
   Friction thermal sca.    tstar :  0.12137E+01 0.48681E+03
   Rough dim-less th. sca.  tplus :  0.25526E-02 0.20791E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26980E+00      10   0.15817E-04   0.58579E+01 0.39142E+02 
c  Velocity[X]                                      0.25732E+01 
c  Velocity[Y]                                      0.15532E+01 
c  Velocity[Z]                                      0.17315E+01 
c  Pressure     0.19725E-04      19   0.36066E-03   0.20243E-01 0.47109E+02 
c  k            0.20625E-01      12   0.65750E-04   0.15186E+00 0.53576E+02 
c  omega        0.27922E+07       1   0.10959E-06   0.23785E+08 0.85272E+00 
c  TempK        0.10046E+05       4   0.48549E-05   0.52982E+01 0.82626E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4374e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.162          19.192    -6.7396e-005       -0.013488
v  Velocity[Y]             -15.063           15.24          0.3065         0.45314
v  Velocity[Z]             -25.177          11.851         -1.6377        -0.50692
v  ǁVelocityǁ         0.00035829          25.584          7.6364          6.5157
v  Pressure                -564.12          189.33          14.083          19.456
v  k                   9.7618e-011          9.3264         0.24825         0.53873
v  omega                    57.498     2.7318e+008     1.2912e+006           76847
v  TempK                     298.6          363.17          338.07          347.06
v  TurbVisc            2.4463e-018       0.0018489     6.3831e-005      0.00022366
v  CourantNb           7.3957e-005          1.5534         0.78812          0.9695
v  FourierNb             0.0038037               1         0.42241         0.19082
v  total_pressure      1.0076e+005     1.0151e+005     1.0134e+005     1.0134e+005
v  Local Time Step          1e-006       0.0038823     7.4266e-005      0.00020317

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9349         0.62774         0.48278


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39997          2.1503          1.2105          1.1603


 INSTANT    0.897000000E-02   TIME STEP NUMBER             897
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925336E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49872E-02 0.46745E+01
   Friction velocity        uk    :  0.49872E-02 0.46705E+01
   Dimensionless distance   yplus :  0.33814E-02 0.29351E+01
   Friction thermal sca.    tstar :  0.12139E+01 0.51877E+03
   Rough dim-less th. sca.  tplus :  0.23954E-02 0.20792E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26977E+00      10   0.15826E-04   0.58810E+01 0.39228E+02 
c  Velocity[X]                                      0.25951E+01 
c  Velocity[Y]                                      0.15522E+01 
c  Velocity[Z]                                      0.17337E+01 
c  Pressure     0.19730E-04      20   0.35355E-03   0.20245E-01 0.48473E+02 
c  k            0.20634E-01      12   0.65590E-04   0.15173E+00 0.53608E+02 
c  omega        0.27922E+07       1   0.10839E-06   0.21037E+08 0.81429E+00 
c  TempK        0.10046E+05       4   0.48554E-05   0.53219E+01 0.82757E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4406e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.165          19.191    -4.8925e-005       -0.013449
v  Velocity[Y]             -14.975          15.235           0.307         0.45384
v  Velocity[Z]             -25.177          11.849         -1.6376        -0.50689
v  ǁVelocityǁ         0.00036462          25.584           7.636          6.5155
v  Pressure                -563.94          189.05          13.812           19.19
v  k                   9.7612e-011          9.4523         0.24839           0.539
v  omega                    57.498     2.7318e+008     1.2912e+006           76847
v  TempK                     298.6          363.17          338.08          347.06
v  TurbVisc            2.4462e-018         0.00185     6.3877e-005      0.00022379
v  CourantNb            0.00010402          1.5526          0.7881         0.96949
v  FourierNb             0.0038035               1         0.42245         0.19088
v  total_pressure      1.0076e+005     1.0151e+005     1.0134e+005     1.0134e+005
v  Local Time Step          1e-006       0.0036702     7.4269e-005      0.00020316

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9351         0.62772         0.48277


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.28892          2.1496          1.2106          1.1604


 INSTANT    0.898000000E-02   TIME STEP NUMBER             898
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925372E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47427E-02 0.46747E+01
   Friction velocity        uk    :  0.47427E-02 0.46708E+01
   Dimensionless distance   yplus :  0.32156E-02 0.29353E+01
   Friction thermal sca.    tstar :  0.12137E+01 0.54551E+03
   Rough dim-less th. sca.  tplus :  0.22780E-02 0.20794E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26975E+00      10   0.15841E-04   0.58984E+01 0.39271E+02 
c  Velocity[X]                                      0.26136E+01 
c  Velocity[Y]                                      0.15476E+01 
c  Velocity[Z]                                      0.17372E+01 
c  Pressure     0.19801E-04      19   0.35419E-03   0.20316E-01 0.49679E+02 
c  k            0.20644E-01      12   0.65186E-04   0.15177E+00 0.53669E+02 
c  omega        0.27922E+07       1   0.10612E-06   0.15041E+08 0.72366E+00 
c  TempK        0.10046E+05       4   0.48557E-05   0.53428E+01 0.82888E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4437e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.168           19.19    -3.0572e-005       -0.013409
v  Velocity[Y]             -14.935          15.231          0.3075         0.45454
v  Velocity[Z]             -25.177          11.847         -1.6376        -0.50685
v  ǁVelocityǁ         0.00037216          25.584          7.6357          6.5152
v  Pressure                -563.74          188.76          13.534          18.917
v  k                   9.7605e-011          9.7397         0.24854         0.53928
v  omega                    57.498     2.7318e+008     1.2912e+006           76847
v  TempK                     298.6          363.17          338.08          347.07
v  TurbVisc             2.446e-018       0.0018515     6.3924e-005      0.00022394
v  CourantNb            0.00011949          1.5519         0.78809         0.96948
v  FourierNb             0.0038032               1          0.4225         0.19095
v  total_pressure      1.0076e+005     1.0151e+005     1.0134e+005     1.0134e+005
v  Local Time Step          1e-006        0.003608     7.4272e-005      0.00020315

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9353         0.62771         0.48277


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47557           2.149          1.2106          1.1604


 INSTANT    0.899000000E-02   TIME STEP NUMBER             899
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925437E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45213E-02 0.46750E+01
   Friction velocity        uk    :  0.45213E-02 0.46711E+01
   Dimensionless distance   yplus :  0.30655E-02 0.29355E+01
   Friction thermal sca.    tstar :  0.12135E+01 0.57222E+03
   Rough dim-less th. sca.  tplus :  0.21717E-02 0.20795E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26972E+00      10   0.15831E-04   0.59187E+01 0.39351E+02 
c  Velocity[X]                                      0.26289E+01 
c  Velocity[Y]                                      0.15472E+01 
c  Velocity[Z]                                      0.17426E+01 
c  Pressure     0.19794E-04      20   0.35918E-03   0.20307E-01 0.51031E+02 
c  k            0.20653E-01      12   0.65186E-04   0.15162E+00 0.53698E+02 
c  omega        0.27922E+07       1   0.10510E-06   0.12021E+08 0.67415E+00 
c  TempK        0.10046E+05       4   0.48556E-05   0.53612E+01 0.83020E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4464e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.17          19.189    -1.2909e-005       -0.013366
v  Velocity[Y]             -14.952          15.226         0.30801         0.45524
v  Velocity[Z]             -25.177          11.845         -1.6376        -0.50682
v  ǁVelocityǁ         0.00038036          25.585          7.6353           6.515
v  Pressure                -563.55          188.46          13.248          18.635
v  k                   9.7599e-011          9.8939         0.24869         0.53957
v  omega                    57.498     2.7318e+008     1.2912e+006           76847
v  TempK                     298.6          363.17          338.08          347.08
v  TurbVisc            2.4458e-018       0.0018625     6.3971e-005      0.00022408
v  CourantNb            0.00012637          1.5512         0.78808         0.96947
v  FourierNb              0.003803               1         0.42254         0.19103
v  total_pressure      1.0076e+005     1.0151e+005     1.0134e+005     1.0134e+005
v  Local Time Step          1e-006       0.0035489     7.4274e-005      0.00020313

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9355         0.62769         0.48276


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57981          2.1484          1.2106          1.1605


 INSTANT    0.900000000E-02   TIME STEP NUMBER             900
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925358E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.42621E-02 0.46753E+01
   Friction velocity        uk    :  0.42620E-02 0.46714E+01
   Dimensionless distance   yplus :  0.28897E-02 0.29356E+01
   Friction thermal sca.    tstar :  0.12135E+01 0.60704E+03
   Rough dim-less th. sca.  tplus :  0.20471E-02 0.20796E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26969E+00      10   0.15834E-04   0.59436E+01 0.39451E+02 
c  Velocity[X]                                      0.26457E+01 
c  Velocity[Y]                                      0.15484E+01 
c  Velocity[Z]                                      0.17495E+01 
c  Pressure     0.19887E-04      19   0.35266E-03   0.20402E-01 0.49885E+02 
c  k            0.20662E-01      12   0.64797E-04   0.15131E+00 0.53697E+02 
c  omega        0.27922E+07       1   0.10600E-06   0.14431E+08 0.71017E+00 
c  TempK        0.10046E+05       4   0.48554E-05   0.53782E+01 0.83164E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4488e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.173          19.188     6.4808e-006       -0.013324
v  Velocity[Y]             -15.045          15.221         0.30853         0.45595
v  Velocity[Z]             -25.178          11.843         -1.6375        -0.50678
v  ǁVelocityǁ         0.00038935          25.585          7.6349          6.5147
v  Pressure                -563.32          188.17           12.97          18.361
v  k                   9.7593e-011          9.9433         0.24884         0.53986
v  omega                    57.498     2.7318e+008     1.2912e+006           76847
v  TempK                     298.6          363.17          338.09          347.09
v  TurbVisc            2.4457e-018        0.001873     6.4018e-005      0.00022423
v  CourantNb            0.00013368          1.5507         0.78807         0.96946
v  FourierNb             0.0038028               1         0.42259          0.1911
v  total_pressure      1.0076e+005     1.0151e+005     1.0134e+005     1.0134e+005
v  Local Time Step          1e-006        0.003494     7.4277e-005      0.00020312

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9356         0.62768         0.48276


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4686          2.1479          1.2107          1.1606


 INSTANT    0.901000000E-02   TIME STEP NUMBER             901
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925392E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.40450E-02 0.46756E+01
   Friction velocity        uk    :  0.40450E-02 0.46717E+01
   Dimensionless distance   yplus :  0.27426E-02 0.29358E+01
   Friction thermal sca.    tstar :  0.12134E+01 0.63961E+03
   Rough dim-less th. sca.  tplus :  0.19429E-02 0.20797E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26967E+00      10   0.15880E-04   0.59662E+01 0.39554E+02 
c  Velocity[X]                                      0.26605E+01 
c  Velocity[Y]                                      0.15496E+01 
c  Velocity[Z]                                      0.17561E+01 
c  Pressure     0.20027E-04      19   0.35098E-03   0.20544E-01 0.50695E+02 
c  k            0.20671E-01      12   0.64282E-04   0.15104E+00 0.53717E+02 
c  omega        0.27922E+07       1   0.10690E-06   0.17627E+08 0.75642E+00 
c  TempK        0.10046E+05       4   0.48554E-05   0.54000E+01 0.83337E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4511e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.176          19.187     2.5679e-005       -0.013287
v  Velocity[Y]             -15.105          15.216         0.30904         0.45665
v  Velocity[Z]             -25.178          12.002         -1.6375        -0.50674
v  ǁVelocityǁ         0.00039892          25.586          7.6346          6.5144
v  Pressure                -563.08          187.87          12.686          18.081
v  k                   9.7587e-011          9.8373         0.24899         0.54015
v  omega                    57.498     2.7318e+008     1.2912e+006           76847
v  TempK                     298.6          363.17          338.09           347.1
v  TurbVisc            2.4455e-018       0.0018782     6.4065e-005      0.00022438
v  CourantNb            0.00012956          1.5501         0.78806         0.96945
v  FourierNb             0.0038026               1         0.42264         0.19118
v  total_pressure      1.0076e+005     1.0151e+005     1.0134e+005     1.0134e+005
v  Local Time Step          1e-006       0.0034439      7.428e-005      0.00020311

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9358         0.62766         0.48275


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4126          2.1474          1.2107          1.1606


 INSTANT    0.902000000E-02   TIME STEP NUMBER             902
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925444E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.38550E-02 0.46759E+01
   Friction velocity        uk    :  0.38550E-02 0.46719E+01
   Dimensionless distance   yplus :  0.26137E-02 0.29360E+01
   Friction thermal sca.    tstar :  0.12133E+01 0.67115E+03
   Rough dim-less th. sca.  tplus :  0.18516E-02 0.20799E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26964E+00      10   0.15812E-04   0.59901E+01 0.39658E+02 
c  Velocity[X]                                      0.26736E+01 
c  Velocity[Y]                                      0.15522E+01 
c  Velocity[Z]                                      0.17643E+01 
c  Pressure     0.20222E-04      20   0.35438E-03   0.20743E-01 0.51785E+02 
c  k            0.20681E-01      12   0.63965E-04   0.15058E+00 0.53695E+02 
c  omega        0.27922E+07       1   0.10817E-06   0.21272E+08 0.80884E+00 
c  TempK        0.10046E+05       4   0.48552E-05   0.54205E+01 0.83485E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4541e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.179          19.186     4.5669e-005       -0.013252
v  Velocity[Y]             -15.045          15.211         0.30956         0.45735
v  Velocity[Z]             -25.178          11.838         -1.6375         -0.5067
v  ǁVelocityǁ         0.00040982          25.586          7.6342          6.5142
v  Pressure                -562.83          187.57          12.396          17.795
v  k                    9.758e-011          9.6805         0.24914         0.54046
v  omega                    57.498     2.7318e+008     1.2912e+006           76847
v  TempK                    298.61          363.17           338.1           347.1
v  TurbVisc            2.4454e-018       0.0018802     6.4112e-005      0.00022452
v  CourantNb            0.00012774          1.5494         0.78804         0.96944
v  FourierNb             0.0038024               1         0.42268         0.19125
v  total_pressure      1.0076e+005     1.0151e+005     1.0134e+005     1.0134e+005
v  Local Time Step          1e-006       0.0033998     7.4282e-005       0.0002031

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0           2.936         0.62765         0.48275


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38699          2.1468          1.2107          1.1607


 INSTANT    0.903000000E-02   TIME STEP NUMBER             903
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925315E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36929E-02 0.46762E+01
   Friction velocity        uk    :  0.36929E-02 0.46722E+01
   Dimensionless distance   yplus :  0.25039E-02 0.29361E+01
   Friction thermal sca.    tstar :  0.12134E+01 0.70061E+03
   Rough dim-less th. sca.  tplus :  0.17738E-02 0.20800E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26961E+00      10   0.15885E-04   0.60076E+01 0.39724E+02 
c  Velocity[X]                                      0.26876E+01 
c  Velocity[Y]                                      0.15523E+01 
c  Velocity[Z]                                      0.17677E+01 
c  Pressure     0.20380E-04      19   0.35106E-03   0.20902E-01 0.51692E+02 
c  k            0.20690E-01      12   0.63714E-04   0.15001E+00 0.53657E+02 
c  omega        0.27922E+07       1   0.10624E-06   0.15902E+08 0.73207E+00 
c  TempK        0.10046E+05       4   0.48548E-05   0.54414E+01 0.83623E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4574e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.182          19.185     6.8583e-005       -0.013213
v  Velocity[Y]             -14.983          15.207         0.31009         0.45806
v  Velocity[Z]             -25.178          11.835         -1.6374        -0.50666
v  ǁVelocityǁ           0.000421          25.586          7.6338          6.5139
v  Pressure                -562.57          187.27          12.107           17.51
v  k                   9.7574e-011          9.7849         0.24929         0.54077
v  omega                    57.498     2.7318e+008     1.2912e+006           76846
v  TempK                    298.61          363.17           338.1          347.11
v  TurbVisc            2.4452e-018       0.0018819      6.416e-005      0.00022467
v  CourantNb            0.00012961          1.5486         0.78803         0.96943
v  FourierNb             0.0038022               1         0.42273         0.19132
v  total_pressure      1.0076e+005     1.0151e+005     1.0134e+005     1.0134e+005
v  Local Time Step          1e-006        0.003363     7.4283e-005      0.00020308

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9361         0.62764         0.48274


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52547          2.1461          1.2108          1.1608


 INSTANT    0.904000000E-02   TIME STEP NUMBER             904
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925405E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36249E-02 0.46765E+01
   Friction velocity        uk    :  0.36249E-02 0.46726E+01
   Dimensionless distance   yplus :  0.24577E-02 0.29363E+01
   Friction thermal sca.    tstar :  0.12134E+01 0.71377E+03
   Rough dim-less th. sca.  tplus :  0.17411E-02 0.20801E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26958E+00      10   0.15897E-04   0.60259E+01 0.39779E+02 
c  Velocity[X]                                      0.27001E+01 
c  Velocity[Y]                                      0.15519E+01 
c  Velocity[Z]                                      0.17739E+01 
c  Pressure     0.20580E-04      19   0.35177E-03   0.21107E-01 0.54720E+02 
c  k            0.20700E-01      12   0.63372E-04   0.14933E+00 0.53610E+02 
c  omega        0.27922E+07       1   0.10613E-06   0.16174E+08 0.73329E+00 
c  TempK        0.10045E+05       4   0.48553E-05   0.54589E+01 0.83714E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4606e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.185          19.185     9.2103e-005       -0.013177
v  Velocity[Y]             -14.964          15.202         0.31062         0.45878
v  Velocity[Z]             -25.179          11.832         -1.6374        -0.50662
v  ǁVelocityǁ          0.0004332          25.587          7.6334          6.5137
v  Pressure                 -562.3          186.95          11.799          17.208
v  k                   9.7568e-011          9.8084         0.24944         0.54108
v  omega                    57.498     2.7318e+008     1.2912e+006           76846
v  TempK                    298.61          363.17          338.11          347.12
v  TurbVisc            2.4451e-018       0.0018834     6.4209e-005      0.00022483
v  CourantNb            0.00013057          1.5478         0.78802         0.96941
v  FourierNb              0.003802               1         0.42277          0.1914
v  total_pressure      1.0076e+005     1.0151e+005     1.0134e+005     1.0134e+005
v  Local Time Step          1e-006       0.0033384     7.4284e-005      0.00020306

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9363         0.62762         0.48273


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52558          2.1454          1.2108          1.1608


 INSTANT    0.905000000E-02   TIME STEP NUMBER             905
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925349E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36586E-02 0.46768E+01
   Friction velocity        uk    :  0.36586E-02 0.46729E+01
   Dimensionless distance   yplus :  0.24806E-02 0.29364E+01
   Friction thermal sca.    tstar :  0.12133E+01 0.70720E+03
   Rough dim-less th. sca.  tplus :  0.17573E-02 0.20802E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26956E+00      10   0.15909E-04   0.60391E+01 0.39825E+02 
c  Velocity[X]                                      0.27089E+01 
c  Velocity[Y]                                      0.15498E+01 
c  Velocity[Z]                                      0.17804E+01 
c  Pressure     0.20790E-04      20   0.35736E-03   0.21322E-01 0.54756E+02 
c  k            0.20709E-01      12   0.63366E-04   0.14876E+00 0.53577E+02 
c  omega        0.27922E+07       1   0.10485E-06   0.13115E+08 0.67739E+00 
c  TempK        0.10045E+05       4   0.48548E-05   0.54572E+01 0.83770E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4633e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.188          19.185      0.00011949       -0.013144
v  Velocity[Y]             -15.037          15.198         0.31116         0.45949
v  Velocity[Z]             -25.179          11.829         -1.6373        -0.50657
v  ǁVelocityǁ         0.00041651          25.588          7.6331          6.5134
v  Pressure                   -562          186.63          11.491          16.904
v  k                   9.7562e-011          9.9113         0.24959          0.5414
v  omega                    57.498     2.7318e+008     1.2912e+006           76846
v  TempK                    298.61          363.17          338.11          347.13
v  TurbVisc            2.4449e-018       0.0018847     6.4257e-005      0.00022499
v  CourantNb            0.00013044          1.5472         0.78801          0.9694
v  FourierNb             0.0038018               1         0.42281         0.19148
v  total_pressure      1.0076e+005     1.0151e+005     1.0134e+005     1.0134e+005
v  Local Time Step          1e-006        0.003332     7.4284e-005      0.00020304

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9364          0.6276         0.48272


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59675          2.1449          1.2108          1.1609


 INSTANT    0.906000000E-02   TIME STEP NUMBER             906
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925361E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37829E-02 0.46771E+01
   Friction velocity        uk    :  0.37829E-02 0.46732E+01
   Dimensionless distance   yplus :  0.25649E-02 0.29365E+01
   Friction thermal sca.    tstar :  0.12131E+01 0.68396E+03
   Rough dim-less th. sca.  tplus :  0.18170E-02 0.20803E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26953E+00      10   0.15905E-04   0.60597E+01 0.39909E+02 
c  Velocity[X]                                      0.27193E+01 
c  Velocity[Y]                                      0.15511E+01 
c  Velocity[Z]                                      0.17894E+01 
c  Pressure     0.21452E-04      20   0.36780E-03   0.22004E-01 0.53990E+02 
c  k            0.20719E-01      12   0.63233E-04   0.14827E+00 0.53543E+02 
c  omega        0.27922E+07       1   0.10587E-06   0.17104E+08 0.73102E+00 
c  TempK        0.10045E+05       4   0.48541E-05   0.54605E+01 0.83849E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4658e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.191          19.184      0.00014857       -0.013118
v  Velocity[Y]             -15.085          15.193          0.3117         0.46022
v  Velocity[Z]              -25.18          11.827         -1.6373        -0.50652
v  ǁVelocityǁ         0.00039776          25.588          7.6327          6.5131
v  Pressure                -561.67          186.31          11.189          16.606
v  k                   9.7556e-011          9.8683         0.24975         0.54173
v  omega                    57.498     2.7318e+008     1.2912e+006           76846
v  TempK                    298.61          363.17          338.12          347.14
v  TurbVisc            2.4448e-018        0.001886     6.4306e-005      0.00022515
v  CourantNb            0.00012968          1.5466           0.788         0.96939
v  FourierNb             0.0038017               1         0.42286         0.19156
v  total_pressure      1.0076e+005     1.0151e+005     1.0134e+005     1.0134e+005
v  Local Time Step          1e-006       0.0033459     7.4285e-005      0.00020302

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52           306.6
v  Yplus               0          2.9365         0.62759         0.48271


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64361          2.1444          1.2109           1.161


 INSTANT    0.907000000E-02   TIME STEP NUMBER             907
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925417E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39264E-02 0.46775E+01
   Friction velocity        uk    :  0.39264E-02 0.46735E+01
   Dimensionless distance   yplus :  0.26621E-02 0.29366E+01
   Friction thermal sca.    tstar :  0.12131E+01 0.65897E+03
   Rough dim-less th. sca.  tplus :  0.18859E-02 0.20803E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26950E+00      10   0.15915E-04   0.60681E+01 0.39967E+02 
c  Velocity[X]                                      0.27255E+01 
c  Velocity[Y]                                      0.15500E+01 
c  Velocity[Z]                                      0.17926E+01 
c  Pressure     0.21195E-04      20   0.35854E-03   0.21741E-01 0.56175E+02 
c  k            0.20729E-01      12   0.63091E-04   0.14777E+00 0.53504E+02 
c  omega        0.27922E+07       1   0.10550E-06   0.17457E+08 0.73365E+00 
c  TempK        0.10045E+05       4   0.48533E-05   0.54536E+01 0.83881E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4691e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.195          19.184      0.00017791       -0.013095
v  Velocity[Y]             -15.038          15.188         0.31224         0.46094
v  Velocity[Z]              -25.18          11.824         -1.6372        -0.50648
v  ǁVelocityǁ          0.0003792          25.589          7.6324          6.5128
v  Pressure                -561.33          185.98          10.873          16.294
v  k                   9.7549e-011          9.9531          0.2499         0.54205
v  omega                    57.498     2.7318e+008     1.2912e+006           76846
v  TempK                    298.61          363.17          338.12          347.15
v  TurbVisc            2.4446e-018       0.0018871     6.4354e-005      0.00022532
v  CourantNb            0.00012798          1.5458         0.78799         0.96938
v  FourierNb             0.0038015               1          0.4229         0.19164
v  total_pressure      1.0076e+005     1.0151e+005     1.0134e+005     1.0134e+005
v  Local Time Step          1e-006       0.0033834     7.4286e-005        0.000203

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52          306.61
v  Yplus               0          2.9366         0.62758         0.48271


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63711          2.1437          1.2109           1.161


 INSTANT    0.908000000E-02   TIME STEP NUMBER             908
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925346E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41265E-02 0.46778E+01
   Friction velocity        uk    :  0.41265E-02 0.46738E+01
   Dimensionless distance   yplus :  0.27978E-02 0.29367E+01
   Friction thermal sca.    tstar :  0.12130E+01 0.62702E+03
   Rough dim-less th. sca.  tplus :  0.19820E-02 0.20804E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26948E+00      10   0.15906E-04   0.60721E+01 0.39991E+02 
c  Velocity[X]                                      0.27309E+01 
c  Velocity[Y]                                      0.15437E+01 
c  Velocity[Z]                                      0.17975E+01 
c  Pressure     0.20454E-04      19   0.35288E-03   0.20983E-01 0.55397E+02 
c  k            0.20739E-01      12   0.62902E-04   0.14746E+00 0.53477E+02 
c  omega        0.27922E+07       1   0.10347E-06   0.12260E+08 0.64183E+00 
c  TempK        0.10045E+05       4   0.48528E-05   0.54558E+01 0.83943E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4726e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.198          19.183      0.00020702       -0.013076
v  Velocity[Y]              -14.99          15.183          0.3128         0.46167
v  Velocity[Z]             -25.181          11.821         -1.6372        -0.50644
v  ǁVelocityǁ         0.00036101          25.589           7.632          6.5126
v  Pressure                -560.99          185.66          10.562          15.988
v  k                   9.7543e-011          10.135         0.25005         0.54239
v  omega                    57.498     2.7318e+008     1.2912e+006           76846
v  TempK                    298.61          363.17          338.12          347.15
v  TurbVisc            2.4444e-018       0.0018882     6.4403e-005      0.00022548
v  CourantNb            0.00012516           1.545         0.78798         0.96938
v  FourierNb             0.0038014               1         0.42295         0.19173
v  total_pressure      1.0076e+005     1.0151e+005     1.0134e+005     1.0134e+005
v  Local Time Step          1e-006       0.0034499     7.4286e-005      0.00020299

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52          306.61
v  Yplus               0          2.9367         0.62757          0.4827


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56575          2.1429          1.2109          1.1611


 INSTANT    0.909000000E-02   TIME STEP NUMBER             909
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925313E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.43969E-02 0.46781E+01
   Friction velocity        uk    :  0.43968E-02 0.46742E+01
   Dimensionless distance   yplus :  0.29811E-02 0.29368E+01
   Friction thermal sca.    tstar :  0.12131E+01 0.58847E+03
   Rough dim-less th. sca.  tplus :  0.21119E-02 0.20805E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26945E+00      10   0.15896E-04   0.60848E+01 0.40061E+02 
c  Velocity[X]                                      0.27380E+01 
c  Velocity[Y]                                      0.15450E+01 
c  Velocity[Z]                                      0.18018E+01 
c  Pressure     0.20452E-04      19   0.35004E-03   0.20983E-01 0.56249E+02 
c  k            0.20750E-01      12   0.62880E-04   0.14694E+00 0.53421E+02 
c  omega        0.27922E+07       1   0.10490E-06   0.18289E+08 0.73837E+00 
c  TempK        0.10045E+05       4   0.48518E-05   0.54638E+01 0.84002E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4759e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.201          19.183      0.00023934       -0.013059
v  Velocity[Y]             -14.981          15.179         0.31336         0.46241
v  Velocity[Z]             -25.181          11.819         -1.6371         -0.5064
v  ǁVelocityǁ         0.00034219           25.59          7.6316          6.5123
v  Pressure                -560.63          185.33          10.247          15.677
v  k                   9.7536e-011          10.126         0.25021         0.54272
v  omega                    57.498     2.7318e+008     1.2912e+006           76846
v  TempK                    298.61          363.17          338.13          347.16
v  TurbVisc            2.4443e-018       0.0018891     6.4452e-005      0.00022566
v  CourantNb            0.00012178          1.5442         0.78797         0.96937
v  FourierNb             0.0038012               1         0.42299         0.19182
v  total_pressure      1.0076e+005     1.0151e+005     1.0134e+005     1.0134e+005
v  Local Time Step          1e-006       0.0035448     7.4287e-005      0.00020297

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52          306.61
v  Yplus               0          2.9368         0.62756         0.48269


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55934          2.1422           1.211          1.1612


 INSTANT    0.910000000E-02   TIME STEP NUMBER             910
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925407E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47014E-02 0.46785E+01
   Friction velocity        uk    :  0.47014E-02 0.46745E+01
   Dimensionless distance   yplus :  0.31876E-02 0.29369E+01
   Friction thermal sca.    tstar :  0.12131E+01 0.55036E+03
   Rough dim-less th. sca.  tplus :  0.22581E-02 0.20805E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26943E+00      10   0.15894E-04   0.60938E+01 0.40081E+02 
c  Velocity[X]                                      0.27434E+01 
c  Velocity[Y]                                      0.15411E+01 
c  Velocity[Z]                                      0.18093E+01 
c  Pressure     0.20576E-04      20   0.35141E-03   0.21113E-01 0.58368E+02 
c  k            0.20760E-01      12   0.63026E-04   0.14651E+00 0.53384E+02 
c  omega        0.27922E+07       1   0.10341E-06   0.13245E+08 0.65658E+00 
c  TempK        0.10045E+05       4   0.48500E-05   0.54697E+01 0.84032E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4788e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.204          19.182      0.00027186       -0.013044
v  Velocity[Y]             -15.003          15.175         0.31392         0.46315
v  Velocity[Z]             -25.182          11.816         -1.6371        -0.50636
v  ǁVelocityǁ         0.00032493          25.591          7.6313           6.512
v  Pressure                -560.25          184.99          9.9183          15.353
v  k                    9.753e-011          10.246         0.25036         0.54306
v  omega                    57.498     2.7318e+008     1.2912e+006           76846
v  TempK                     298.6          363.17          338.13          347.17
v  TurbVisc            2.4441e-018       0.0018898     6.4501e-005      0.00022583
v  CourantNb            0.00013138          1.5435         0.78797         0.96936
v  FourierNb             0.0038011               1         0.42304         0.19191
v  total_pressure      1.0076e+005     1.0151e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0035901     7.4289e-005      0.00020296

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52          306.61
v  Yplus               0          2.9369         0.62755         0.48268


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46654          2.1417           1.211          1.1613


 INSTANT    0.911000000E-02   TIME STEP NUMBER             911
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925364E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48740E-02 0.46788E+01
   Friction velocity        uk    :  0.48740E-02 0.46749E+01
   Dimensionless distance   yplus :  0.33047E-02 0.29370E+01
   Friction thermal sca.    tstar :  0.12129E+01 0.53087E+03
   Rough dim-less th. sca.  tplus :  0.23410E-02 0.20806E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26940E+00      10   0.15977E-04   0.61120E+01 0.40130E+02 
c  Velocity[X]                                      0.27482E+01 
c  Velocity[Y]                                      0.15391E+01 
c  Velocity[Z]                                      0.18246E+01 
c  Pressure     0.21225E-04      19   0.35374E-03   0.21782E-01 0.57623E+02 
c  k            0.20771E-01      12   0.62881E-04   0.14612E+00 0.53350E+02 
c  omega        0.27922E+07       1   0.10340E-06   0.12515E+08 0.64034E+00 
c  TempK        0.10044E+05       4   0.48487E-05   0.54737E+01 0.84066E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4813e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.208          19.182      0.00030747       -0.013037
v  Velocity[Y]             -15.116           15.17         0.31449          0.4639
v  Velocity[Z]             -25.183          11.813          -1.637        -0.50632
v  ǁVelocityǁ         0.00030816          25.591          7.6309          6.5117
v  Pressure                -559.86          184.65          9.5948          15.034
v  k                   9.7523e-011          10.243         0.25052          0.5434
v  omega                    57.499     2.7318e+008     1.2912e+006           76845
v  TempK                     298.6          363.17          338.14          347.18
v  TurbVisc             2.444e-018       0.0018904     6.4551e-005        0.000226
v  CourantNb            0.00014154          1.5429         0.78796         0.96935
v  FourierNb             0.0038009               1         0.42309         0.19201
v  total_pressure      1.0077e+005     1.0151e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0036414     7.4291e-005      0.00020295

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52          306.61
v  Yplus               0           2.937         0.62753         0.48267


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52878          2.1412           1.211          1.1614


 INSTANT    0.912000000E-02   TIME STEP NUMBER             912
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925284E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51018E-02 0.46792E+01
   Friction velocity        uk    :  0.51018E-02 0.46752E+01
   Dimensionless distance   yplus :  0.34591E-02 0.29370E+01
   Friction thermal sca.    tstar :  0.12127E+01 0.50717E+03
   Rough dim-less th. sca.  tplus :  0.24505E-02 0.20806E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26938E+00      10   0.16064E-04   0.61176E+01 0.40180E+02 
c  Velocity[X]                                      0.27515E+01 
c  Velocity[Y]                                      0.15400E+01 
c  Velocity[Z]                                      0.18261E+01 
c  Pressure     0.20894E-04      19   0.35400E-03   0.21446E-01 0.56810E+02 
c  k            0.20782E-01      12   0.62812E-04   0.14584E+00 0.53310E+02 
c  omega        0.27922E+07       1   0.10808E-06   0.27802E+08 0.87210E+00 
c  TempK        0.10044E+05       4   0.48476E-05   0.54807E+01 0.84109E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4839e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.211          19.181      0.00034432       -0.013031
v  Velocity[Y]             -15.163          15.165         0.31505         0.46466
v  Velocity[Z]             -25.183          11.811          -1.637        -0.50629
v  ǁVelocityǁ         0.00029196          25.592          7.6305          6.5114
v  Pressure                -559.41          184.32          9.2768           14.72
v  k                   9.7517e-011          10.066         0.25067         0.54375
v  omega                    57.499     2.7318e+008     1.2912e+006           76845
v  TempK                     298.6          363.17          338.14          347.18
v  TurbVisc            2.4438e-018        0.001891     6.4599e-005      0.00022617
v  CourantNb            0.00015168          1.5423         0.78795         0.96934
v  FourierNb             0.0038008               1         0.42313          0.1921
v  total_pressure      1.0077e+005     1.0151e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0037171     7.4293e-005      0.00020294

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52          306.61
v  Yplus               0           2.937         0.62752         0.48266


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45326          2.1406          1.2111          1.1614


 INSTANT    0.913000000E-02   TIME STEP NUMBER             913
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925404E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53182E-02 0.46795E+01
   Friction velocity        uk    :  0.53182E-02 0.46756E+01
   Dimensionless distance   yplus :  0.36058E-02 0.29371E+01
   Friction thermal sca.    tstar :  0.12127E+01 0.48653E+03
   Rough dim-less th. sca.  tplus :  0.25544E-02 0.20807E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26935E+00      10   0.16097E-04   0.61255E+01 0.40213E+02 
c  Velocity[X]                                      0.27523E+01 
c  Velocity[Y]                                      0.15387E+01 
c  Velocity[Z]                                      0.18346E+01 
c  Pressure     0.20841E-04      20   0.35553E-03   0.21396E-01 0.57604E+02 
c  k            0.20792E-01      12   0.63127E-04   0.14563E+00 0.53290E+02 
c  omega        0.27922E+07       1   0.10460E-06   0.15260E+08 0.69766E+00 
c  TempK        0.10044E+05       4   0.48463E-05   0.54883E+01 0.84113E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4873e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.214          19.181       0.0003798       -0.013025
v  Velocity[Y]             -15.078          15.161         0.31562         0.46542
v  Velocity[Z]             -25.184           11.81         -1.6369        -0.50626
v  ǁVelocityǁ         0.00027666          25.593          7.6302          6.5112
v  Pressure                -558.99          183.98          8.9534          14.401
v  k                    9.751e-011          10.094         0.25083         0.54409
v  omega                    57.499     2.7318e+008     1.2912e+006           76845
v  TempK                     298.6          363.17          338.15          347.19
v  TurbVisc            2.4436e-018       0.0018916     6.4648e-005      0.00022635
v  CourantNb            0.00016161          1.5415         0.78794         0.96933
v  FourierNb             0.0038007               1         0.42318          0.1922
v  total_pressure      1.0077e+005     1.0151e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0038154     7.4295e-005      0.00020293

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52          306.61
v  Yplus               0          2.9371         0.62751         0.48265


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35393            2.14          1.2111          1.1615


 INSTANT    0.914000000E-02   TIME STEP NUMBER             914
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925371E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.55415E-02 0.46799E+01
   Friction velocity        uk    :  0.55415E-02 0.46759E+01
   Dimensionless distance   yplus :  0.37572E-02 0.29371E+01
   Friction thermal sca.    tstar :  0.12126E+01 0.46693E+03
   Rough dim-less th. sca.  tplus :  0.26617E-02 0.20807E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26933E+00      10   0.16163E-04   0.61256E+01 0.40213E+02 
c  Velocity[X]                                      0.27540E+01 
c  Velocity[Y]                                      0.15325E+01 
c  Velocity[Z]                                      0.18391E+01 
c  Pressure     0.20683E-04      20   0.35787E-03   0.21239E-01 0.58044E+02 
c  k            0.20803E-01      12   0.63390E-04   0.14554E+00 0.53274E+02 
c  omega        0.27922E+07       1   0.10369E-06   0.12185E+08 0.64107E+00 
c  TempK        0.10044E+05       4   0.48448E-05   0.54905E+01 0.84116E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4908e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.218           19.18      0.00041646       -0.013021
v  Velocity[Y]             -15.021          15.157         0.31619          0.4662
v  Velocity[Z]             -25.185          11.905         -1.6369        -0.50623
v  ǁVelocityǁ         0.00026147          25.594          7.6298          6.5109
v  Pressure                -558.54          183.64           8.628           14.08
v  k                   9.7503e-011           10.05         0.25098         0.54444
v  omega                    57.499     2.7318e+008     1.2912e+006           76845
v  TempK                     298.6          363.17          338.15           347.2
v  TurbVisc            2.4435e-018       0.0018922     6.4696e-005      0.00022652
v  CourantNb            0.00017115          1.5406         0.78793         0.96932
v  FourierNb             0.0038006               1         0.42322          0.1923
v  total_pressure      1.0077e+005     1.0151e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0032205     7.4297e-005      0.00020292

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52          306.61
v  Yplus               0          2.9371          0.6275         0.48264


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60763          2.1392          1.2112          1.1616


 INSTANT    0.915000000E-02   TIME STEP NUMBER             915
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925306E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57814E-02 0.46803E+01
   Friction velocity        uk    :  0.57814E-02 0.46763E+01
   Dimensionless distance   yplus :  0.39199E-02 0.29371E+01
   Friction thermal sca.    tstar :  0.12126E+01 0.44756E+03
   Rough dim-less th. sca.  tplus :  0.27769E-02 0.20807E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26930E+00      10   0.16196E-04   0.61307E+01 0.40249E+02 
c  Velocity[X]                                      0.27563E+01 
c  Velocity[Y]                                      0.15335E+01 
c  Velocity[Z]                                      0.18410E+01 
c  Pressure     0.20577E-04      19   0.35977E-03   0.21136E-01 0.56617E+02 
c  k            0.20814E-01      12   0.63511E-04   0.14552E+00 0.53269E+02 
c  omega        0.27922E+07       1   0.10455E-06   0.15127E+08 0.68997E+00 
c  TempK        0.10044E+05       4   0.48425E-05   0.54825E+01 0.84087E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4941e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.221          19.179      0.00045281       -0.013022
v  Velocity[Y]             -15.015          15.153         0.31676         0.46697
v  Velocity[Z]             -25.186          12.038         -1.6368         -0.5062
v  ǁVelocityǁ         0.00024854          25.595          7.6294          6.5106
v  Pressure                -558.09          183.31          8.3117          13.768
v  k                   9.7496e-011          10.079         0.25114          0.5448
v  omega                    57.499     2.7318e+008     1.2912e+006           76845
v  TempK                     298.6          363.17          338.15          347.21
v  TurbVisc            2.4433e-018       0.0018929     6.4745e-005       0.0002267
v  CourantNb            0.00018724          1.5399         0.78792         0.96931
v  FourierNb             0.0038005               1         0.42327         0.19239
v  total_pressure      1.0077e+005     1.0151e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0032233     7.4298e-005      0.00020291

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52          306.61
v  Yplus               0          2.9371         0.62749         0.48263


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4262          2.1386          1.2112          1.1617


 INSTANT    0.916000000E-02   TIME STEP NUMBER             916
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925391E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60325E-02 0.46806E+01
   Friction velocity        uk    :  0.60324E-02 0.46767E+01
   Dimensionless distance   yplus :  0.40901E-02 0.29372E+01
   Friction thermal sca.    tstar :  0.12127E+01 0.42894E+03
   Rough dim-less th. sca.  tplus :  0.28974E-02 0.20807E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26928E+00      10   0.16150E-04   0.61319E+01 0.40255E+02 
c  Velocity[X]                                      0.27547E+01 
c  Velocity[Y]                                      0.15295E+01 
c  Velocity[Z]                                      0.18477E+01 
c  Pressure     0.20402E-04      20   0.35969E-03   0.20962E-01 0.58960E+02 
c  k            0.20825E-01      12   0.63742E-04   0.14560E+00 0.53276E+02 
c  omega        0.27922E+07       1   0.10549E-06   0.17796E+08 0.72646E+00 
c  TempK        0.10044E+05       4   0.48396E-05   0.54758E+01 0.84047E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4968e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.224          19.178      0.00048994       -0.013026
v  Velocity[Y]             -15.097          15.149         0.31733         0.46775
v  Velocity[Z]             -25.187          12.148         -1.6368        -0.50618
v  ǁVelocityǁ         0.00023687          25.596           7.629          6.5103
v  Pressure                -557.62          182.97           7.981          13.441
v  k                    9.749e-011          10.187         0.25129         0.54515
v  omega                    57.499     2.7318e+008     1.2912e+006           76845
v  TempK                     298.6          363.17          338.16          347.22
v  TurbVisc            2.4431e-018       0.0018943     6.4793e-005      0.00022688
v  CourantNb            0.00020936          1.5392         0.78792         0.96929
v  FourierNb             0.0038004               1         0.42331         0.19249
v  total_pressure      1.0077e+005     1.0151e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0030112     7.4299e-005       0.0002029

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52          306.61
v  Yplus               0          2.9372         0.62747         0.48263


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46006           2.138          1.2112          1.1618


 INSTANT    0.917000000E-02   TIME STEP NUMBER             917
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925304E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62026E-02 0.46810E+01
   Friction velocity        uk    :  0.62026E-02 0.46770E+01
   Dimensionless distance   yplus :  0.42055E-02 0.29372E+01
   Friction thermal sca.    tstar :  0.12125E+01 0.41718E+03
   Rough dim-less th. sca.  tplus :  0.29792E-02 0.20807E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26925E+00      10   0.16215E-04   0.61437E+01 0.40271E+02 
c  Velocity[X]                                      0.27577E+01 
c  Velocity[Y]                                      0.15279E+01 
c  Velocity[Z]                                      0.18582E+01 
c  Pressure     0.20656E-04      19   0.35876E-03   0.21230E-01 0.57618E+02 
c  k            0.20836E-01      12   0.64041E-04   0.14593E+00 0.53303E+02 
c  omega        0.27922E+07       1   0.10496E-06   0.16763E+08 0.70571E+00 
c  TempK        0.10044E+05       4   0.48367E-05   0.54678E+01 0.84007E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4994e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.228          19.177      0.00052441        -0.01303
v  Velocity[Y]             -15.148          15.144          0.3179         0.46853
v  Velocity[Z]             -25.188          12.086         -1.6367        -0.50615
v  ǁVelocityǁ         0.00022726          25.597          7.6287            6.51
v  Pressure                -557.13          182.63          7.6587          13.122
v  k                   9.7483e-011           10.14         0.25145          0.5455
v  omega                    57.499     2.7318e+008     1.2912e+006           76845
v  TempK                     298.6          363.17          338.16          347.22
v  TurbVisc            2.4429e-018       0.0018999     6.4842e-005      0.00022706
v  CourantNb            0.00021841          1.5386         0.78791         0.96928
v  FourierNb             0.0038003               1         0.42336         0.19259
v  total_pressure      1.0077e+005     1.0151e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0028722       7.43e-005      0.00020289

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52          306.61
v  Yplus               0          2.9372         0.62746         0.48262


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39736          2.1375          1.2113          1.1619


 INSTANT    0.918000000E-02   TIME STEP NUMBER             918
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925352E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63863E-02 0.46814E+01
   Friction velocity        uk    :  0.63863E-02 0.46774E+01
   Dimensionless distance   yplus :  0.43300E-02 0.29371E+01
   Friction thermal sca.    tstar :  0.12123E+01 0.40518E+03
   Rough dim-less th. sca.  tplus :  0.30674E-02 0.20807E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26923E+00      10   0.16261E-04   0.61477E+01 0.40289E+02 
c  Velocity[X]                                      0.27584E+01 
c  Velocity[Y]                                      0.15274E+01 
c  Velocity[Z]                                      0.18620E+01 
c  Pressure     0.20426E-04      20   0.36023E-03   0.20999E-01 0.57855E+02 
c  k            0.20848E-01      12   0.64677E-04   0.14657E+00 0.53362E+02 
c  omega        0.27922E+07       1   0.10498E-06   0.16887E+08 0.71046E+00 
c  TempK        0.10044E+05       4   0.48335E-05   0.54605E+01 0.83947E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5027e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.231          19.176      0.00055681        -0.01304
v  Velocity[Y]             -15.098           15.14         0.31847         0.46933
v  Velocity[Z]             -25.189          11.814         -1.6367        -0.50612
v  ǁVelocityǁ          0.0002192          25.598          7.6283          6.5097
v  Pressure                -556.66          182.29          7.3347          12.802
v  k                   9.7476e-011          10.214          0.2516         0.54586
v  omega                    57.499     2.7318e+008     1.2912e+006           76845
v  TempK                    298.61          363.17          338.17          347.23
v  TurbVisc            2.4428e-018       0.0019055     6.4892e-005      0.00022724
v  CourantNb            0.00021902          1.5378          0.7879         0.96926
v  FourierNb             0.0038002               1         0.42341          0.1927
v  total_pressure      1.0077e+005     1.0151e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0031595     7.4302e-005      0.00020289

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52          306.61
v  Yplus               0          2.9371         0.62745         0.48261


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39287          2.1369          1.2113           1.162


 INSTANT    0.919000000E-02   TIME STEP NUMBER             919
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925315E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65636E-02 0.46817E+01
   Friction velocity        uk    :  0.65635E-02 0.46778E+01
   Dimensionless distance   yplus :  0.44502E-02 0.29371E+01
   Friction thermal sca.    tstar :  0.12123E+01 0.39424E+03
   Rough dim-less th. sca.  tplus :  0.31526E-02 0.20807E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         54 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26921E+00      10   0.16306E-04   0.61430E+01 0.40263E+02 
c  Velocity[X]                                      0.27577E+01 
c  Velocity[Y]                                      0.15239E+01 
c  Velocity[Z]                                      0.18614E+01 
c  Pressure     0.20371E-04      19   0.37051E-03   0.20948E-01 0.57276E+02 
c  k            0.20859E-01      12   0.65340E-04   0.14741E+00 0.53463E+02 
c  omega        0.27922E+07       1   0.10255E-06   0.96486E+07 0.58468E+00 
c  TempK        0.10044E+05       4   0.48302E-05   0.54601E+01 0.83915E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5063e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.234          19.175      0.00058436       -0.013055
v  Velocity[Y]             -15.046          15.136         0.31904         0.47013
v  Velocity[Z]              -25.19           12.44         -1.6366         -0.5061
v  ǁVelocityǁ         0.00021396          25.599          7.6279          6.5094
v  Pressure                -556.17          181.95          7.0139          12.486
v  k                   9.7469e-011           10.38         0.25176         0.54621
v  omega                    57.499     2.7319e+008     1.2912e+006           76845
v  TempK                    298.61          363.17          338.17          347.24
v  TurbVisc            2.4426e-018       0.0019114     6.4941e-005      0.00022743
v  CourantNb             0.0002197           1.537         0.78789         0.96925
v  FourierNb             0.0038001               1         0.42346          0.1928
v  total_pressure      1.0077e+005     1.0151e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0034754     7.4303e-005      0.00020288

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52          306.61
v  Yplus               0          2.9371         0.62744          0.4826


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39155          2.1361          1.2113           1.162


 INSTANT    0.920000000E-02   TIME STEP NUMBER             920
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925309E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67610E-02 0.46821E+01
   Friction velocity        uk    :  0.67610E-02 0.46781E+01
   Dimensionless distance   yplus :  0.45841E-02 0.29371E+01
   Friction thermal sca.    tstar :  0.12122E+01 0.38273E+03
   Rough dim-less th. sca.  tplus :  0.32474E-02 0.20807E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26919E+00      10   0.16427E-04   0.61509E+01 0.40281E+02 
c  Velocity[X]                                      0.27574E+01 
c  Velocity[Y]                                      0.15252E+01 
c  Velocity[Z]                                      0.18683E+01 
c  Pressure     0.20361E-04      19   0.37379E-03   0.20943E-01 0.56824E+02 
c  k            0.20870E-01      12   0.66018E-04   0.14856E+00 0.53602E+02 
c  omega        0.27922E+07       1   0.10314E-06   0.11458E+08 0.61511E+00 
c  TempK        0.10043E+05       4   0.48264E-05   0.54605E+01 0.83896E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5096e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.238          19.173      0.00061203       -0.013073
v  Velocity[Y]             -15.033          15.133         0.31961         0.47094
v  Velocity[Z]             -25.191           12.59         -1.6366        -0.50608
v  ǁVelocityǁ         0.00021097          25.601          7.6276          6.5091
v  Pressure                -555.66          181.62          6.6966          12.173
v  k                   9.7462e-011          10.422         0.25191         0.54656
v  omega                    57.499     2.7319e+008     1.2912e+006           76844
v  TempK                    298.61          363.17          338.18          347.25
v  TurbVisc            2.4424e-018       0.0019173     6.4991e-005      0.00022761
v  CourantNb             0.0002203          1.5362         0.78789         0.96923
v  FourierNb                0.0038               1          0.4235          0.1929
v  total_pressure      1.0077e+005     1.0151e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0038229     7.4305e-005      0.00020287

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.52          306.61
v  Yplus               0          2.9371         0.62743         0.48259


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54278          2.1355          1.2114          1.1621


 INSTANT    0.921000000E-02   TIME STEP NUMBER             921
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925307E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69455E-02 0.46825E+01
   Friction velocity        uk    :  0.69455E-02 0.46785E+01
   Dimensionless distance   yplus :  0.47092E-02 0.29370E+01
   Friction thermal sca.    tstar :  0.12123E+01 0.37257E+03
   Rough dim-less th. sca.  tplus :  0.33360E-02 0.20806E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26916E+00      10   0.16881E-04   0.61659E+01 0.40323E+02 
c  Velocity[X]                                      0.27578E+01 
c  Velocity[Y]                                      0.15300E+01 
c  Velocity[Z]                                      0.18781E+01 
c  Pressure     0.20255E-04      19   0.37469E-03   0.20839E-01 0.56051E+02 
c  k            0.20881E-01      12   0.66739E-04   0.14996E+00 0.53778E+02 
c  omega        0.27922E+07       1   0.10418E-06   0.15071E+08 0.67643E+00 
c  TempK        0.10043E+05       4   0.48219E-05   0.54564E+01 0.83859E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5124e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.241          19.172      0.00063892       -0.013095
v  Velocity[Y]             -15.051          15.129         0.32019         0.47176
v  Velocity[Z]             -25.192          12.561         -1.6365        -0.50605
v  ǁVelocityǁ         0.00021087          25.602          7.6272          6.5088
v  Pressure                -555.12           181.3          6.3842          11.864
v  k                   9.7455e-011          10.447         0.25206         0.54692
v  omega                    57.499     2.7319e+008     1.2912e+006           76844
v  TempK                    298.61          363.17          338.18          347.25
v  TurbVisc            2.4423e-018       0.0019233     6.5039e-005      0.00022779
v  CourantNb            0.00022101          1.5355         0.78788         0.96922
v  FourierNb             0.0037999               1         0.42355         0.19301
v  total_pressure      1.0077e+005     1.0151e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0041031     7.4307e-005      0.00020288

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.61
v  Yplus               0           2.937         0.62742         0.48257


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43802          2.1349          1.2114          1.1622


 INSTANT    0.922000000E-02   TIME STEP NUMBER             922
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925276E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71736E-02 0.46829E+01
   Friction velocity        uk    :  0.71736E-02 0.46789E+01
   Dimensionless distance   yplus :  0.48638E-02 0.29370E+01
   Friction thermal sca.    tstar :  0.12123E+01 0.36072E+03
   Rough dim-less th. sca.  tplus :  0.34456E-02 0.20806E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26914E+00      10   0.16994E-04   0.61714E+01 0.40329E+02 
c  Velocity[X]                                      0.27550E+01 
c  Velocity[Y]                                      0.15296E+01 
c  Velocity[Z]                                      0.18868E+01 
c  Pressure     0.20317E-04      19   0.36194E-03   0.20907E-01 0.56701E+02 
c  k            0.20892E-01      12   0.67657E-04   0.15196E+00 0.54051E+02 
c  omega        0.27922E+07       1   0.10537E-06   0.18000E+08 0.71809E+00 
c  TempK        0.10043E+05       4   0.48171E-05   0.54553E+01 0.83815E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5148e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.244           19.17      0.00066529       -0.013119
v  Velocity[Y]              -15.16          15.125         0.32076         0.47258
v  Velocity[Z]             -25.194          12.494         -1.6365        -0.50603
v  ǁVelocityǁ         0.00021357          25.603          7.6268          6.5084
v  Pressure                -554.55          180.97          6.0681          11.552
v  k                   9.7448e-011          10.371         0.25221         0.54727
v  omega                    57.499     2.7319e+008     1.2912e+006           76844
v  TempK                    298.62          363.17          338.18          347.26
v  TurbVisc            2.4421e-018       0.0019293     6.5087e-005      0.00022796
v  CourantNb            0.00022163           1.535         0.78788         0.96921
v  FourierNb             0.0037998               1         0.42359         0.19312
v  total_pressure      1.0077e+005     1.0151e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006        0.003074     7.4309e-005      0.00020288

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.61
v  Yplus               0           2.937         0.62741         0.48256


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41437          2.1345          1.2115          1.1623


 INSTANT    0.923000000E-02   TIME STEP NUMBER             923
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925330E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72881E-02 0.46832E+01
   Friction velocity        uk    :  0.72881E-02 0.46793E+01
   Dimensionless distance   yplus :  0.49414E-02 0.29369E+01
   Friction thermal sca.    tstar :  0.12122E+01 0.35506E+03
   Rough dim-less th. sca.  tplus :  0.35006E-02 0.20805E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26912E+00      10   0.16911E-04   0.61818E+01 0.40317E+02 
c  Velocity[X]                                      0.27544E+01 
c  Velocity[Y]                                      0.15305E+01 
c  Velocity[Z]                                      0.18969E+01 
c  Pressure     0.20616E-04      19   0.35897E-03   0.21218E-01 0.55788E+02 
c  k            0.20903E-01      12   0.68554E-04   0.15406E+00 0.54271E+02 
c  omega        0.27922E+07       1   0.10734E-06   0.27255E+08 0.84743E+00 
c  TempK        0.10043E+05       4   0.48122E-05   0.54522E+01 0.83781E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5173e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.247          19.168      0.00069264       -0.013144
v  Velocity[Y]             -15.203          15.122         0.32133         0.47341
v  Velocity[Z]             -25.195           12.43         -1.6365        -0.50601
v  ǁVelocityǁ         0.00021886          25.605          7.6265          6.5081
v  Pressure                -553.97          180.64          5.7576          11.245
v  k                   9.7442e-011          10.151         0.25236         0.54762
v  omega                    57.499     2.7319e+008     1.2912e+006           76844
v  TempK                    298.62          363.17          338.19          347.27
v  TurbVisc            2.4419e-018       0.0019353     6.5136e-005      0.00022814
v  CourantNb            0.00022229          1.5344         0.78787          0.9692
v  FourierNb             0.0037997               1         0.42364         0.19324
v  total_pressure      1.0077e+005     1.0151e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0027303     7.4312e-005      0.00020288

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.61
v  Yplus               0          2.9369          0.6274         0.48255


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35994           2.134          1.2115          1.1624


 INSTANT    0.924000000E-02   TIME STEP NUMBER             924
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925366E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.74577E-02 0.46836E+01
   Friction velocity        uk    :  0.74577E-02 0.46796E+01
   Dimensionless distance   yplus :  0.50564E-02 0.29368E+01
   Friction thermal sca.    tstar :  0.12120E+01 0.34698E+03
   Rough dim-less th. sca.  tplus :  0.35820E-02 0.20805E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26910E+00      10   0.17102E-04   0.61878E+01 0.40306E+02 
c  Velocity[X]                                      0.27497E+01 
c  Velocity[Y]                                      0.15325E+01 
c  Velocity[Z]                                      0.19056E+01 
c  Pressure     0.20933E-04      19   0.36057E-03   0.21549E-01 0.56257E+02 
c  k            0.20914E-01      12   0.69620E-04   0.15623E+00 0.54526E+02 
c  omega        0.27922E+07       1   0.10362E-06   0.14911E+08 0.66640E+00 
c  TempK        0.10043E+05       4   0.48073E-05   0.54489E+01 0.83722E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5206e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.25          19.166       0.0007223       -0.013174
v  Velocity[Y]             -15.117          15.118          0.3219         0.47425
v  Velocity[Z]             -25.196          12.373         -1.6364        -0.50598
v  ǁVelocityǁ         0.00022704          25.606          7.6261          6.5078
v  Pressure                -553.36          180.32          5.4438          10.935
v  k                   9.7435e-011          10.169         0.25251         0.54798
v  omega                    57.499     2.7319e+008     1.2912e+006           76844
v  TempK                    298.62          363.17          338.19          347.28
v  TurbVisc            2.4417e-018        0.001941     6.5184e-005      0.00022833
v  CourantNb            0.00022293          1.5336         0.78786         0.96918
v  FourierNb             0.0037996               1         0.42369         0.19335
v  total_pressure      1.0077e+005     1.0151e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0025672     7.4315e-005      0.00020288

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.61
v  Yplus               0          2.9368         0.62739         0.48253


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35821          2.1334          1.2115          1.1625


 INSTANT    0.925000000E-02   TIME STEP NUMBER             925
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925270E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75837E-02 0.46840E+01
   Friction velocity        uk    :  0.75837E-02 0.46800E+01
   Dimensionless distance   yplus :  0.51419E-02 0.29367E+01
   Friction thermal sca.    tstar :  0.12120E+01 0.34122E+03
   Rough dim-less th. sca.  tplus :  0.36425E-02 0.20804E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         55 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26908E+00      10   0.17067E-04   0.61805E+01 0.40253E+02 
c  Velocity[X]                                      0.27421E+01 
c  Velocity[Y]                                      0.15305E+01 
c  Velocity[Z]                                      0.19080E+01 
c  Pressure     0.20550E-04      19   0.36381E-03   0.21160E-01 0.54955E+02 
c  k            0.20925E-01      12   0.70834E-04   0.15873E+00 0.54828E+02 
c  omega        0.27922E+07       1   0.10200E-06   0.99541E+07 0.57400E+00 
c  TempK        0.10043E+05       4   0.48029E-05   0.54502E+01 0.83698E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.524e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.164      0.00075193       -0.013203
v  Velocity[Y]             -15.063          15.115         0.32247          0.4751
v  Velocity[Z]             -25.197          12.317         -1.6364        -0.50596
v  ǁVelocityǁ         0.00023666          25.607          7.6257          6.5075
v  Pressure                -552.76             180          5.1379          10.633
v  k                   9.7428e-011           10.33         0.25266         0.54832
v  omega                      57.5     2.7319e+008     1.2912e+006           76844
v  TempK                    298.62          363.17           338.2          347.28
v  TurbVisc            2.4416e-018        0.001946     6.5232e-005      0.00022851
v  CourantNb            0.00022363          1.5328         0.78786         0.96916
v  FourierNb             0.0037995               1         0.42373         0.19346
v  total_pressure      1.0077e+005      1.015e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0026211     7.4318e-005      0.00020289

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.61
v  Yplus               0          2.9367         0.62737         0.48252


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50577          2.1327          1.2116          1.1626


 INSTANT    0.926000000E-02   TIME STEP NUMBER             926
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925192E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77417E-02 0.46843E+01
   Friction velocity        uk    :  0.77417E-02 0.46804E+01
   Dimensionless distance   yplus :  0.52490E-02 0.29366E+01
   Friction thermal sca.    tstar :  0.12119E+01 0.33426E+03
   Rough dim-less th. sca.  tplus :  0.37184E-02 0.20803E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26906E+00      10   0.17182E-04   0.61838E+01 0.40241E+02 
c  Velocity[X]                                      0.27339E+01 
c  Velocity[Y]                                      0.15327E+01 
c  Velocity[Z]                                      0.19172E+01 
c  Pressure     0.20440E-04      19   0.36819E-03   0.21053E-01 0.53589E+02 
c  k            0.20935E-01      12   0.72092E-04   0.16144E+00 0.55164E+02 
c  omega        0.27922E+07       1   0.10240E-06   0.11482E+08 0.59724E+00 
c  TempK        0.10043E+05       4   0.47983E-05   0.54519E+01 0.83688E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5271e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.162      0.00078431       -0.013233
v  Velocity[Y]             -15.059          15.112         0.32303         0.47595
v  Velocity[Z]             -25.199          12.258         -1.6364        -0.50594
v  ǁVelocityǁ         0.00024936          25.609          7.6254          6.5072
v  Pressure                -552.15          179.69           4.841           10.34
v  k                   9.7421e-011          10.404          0.2528         0.54867
v  omega                      57.5     2.7319e+008     1.2912e+006           76844
v  TempK                    298.62          363.17           338.2          347.29
v  TurbVisc            2.4414e-018       0.0019501     6.5278e-005      0.00022869
v  CourantNb            0.00022424          1.5321         0.78785         0.96914
v  FourierNb             0.0037994               1         0.42377         0.19357
v  total_pressure      1.0077e+005      1.015e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0028295     7.4322e-005      0.00020289

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.61
v  Yplus               0          2.9366         0.62736         0.48251


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55751          2.1321          1.2116          1.1627


 INSTANT    0.927000000E-02   TIME STEP NUMBER             927
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925292E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78972E-02 0.46847E+01
   Friction velocity        uk    :  0.78972E-02 0.46807E+01
   Dimensionless distance   yplus :  0.53544E-02 0.29365E+01
   Friction thermal sca.    tstar :  0.12120E+01 0.32768E+03
   Rough dim-less th. sca.  tplus :  0.37931E-02 0.20802E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26904E+00      10   0.17228E-04   0.61943E+01 0.40254E+02 
c  Velocity[X]                                      0.27277E+01 
c  Velocity[Y]                                      0.15397E+01 
c  Velocity[Z]                                      0.19269E+01 
c  Pressure     0.20691E-04      19   0.36232E-03   0.21319E-01 0.53010E+02 
c  k            0.20946E-01      12   0.73725E-04   0.16431E+00 0.55519E+02 
c  omega        0.27922E+07       1   0.10420E-06   0.16954E+08 0.68901E+00 
c  TempK        0.10042E+05       4   0.47941E-05   0.54494E+01 0.83668E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5297e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.259           19.16      0.00082022       -0.013261
v  Velocity[Y]             -15.123           15.11         0.32359         0.47681
v  Velocity[Z]             -25.201          12.196         -1.6364        -0.50592
v  ǁVelocityǁ         0.00026316           25.61           7.625          6.5068
v  Pressure                -551.58          179.39          4.5478           10.05
v  k                   9.7415e-011          10.418         0.25295         0.54901
v  omega                      57.5     2.7319e+008     1.2912e+006           76844
v  TempK                    298.62          363.17           338.2           347.3
v  TurbVisc            2.4412e-018       0.0019599     6.5323e-005      0.00022886
v  CourantNb            0.00010135          1.5315         0.78784         0.96913
v  FourierNb             0.0037993               1         0.42382         0.19368
v  total_pressure      1.0077e+005      1.015e+005     1.0133e+005     1.0134e+005
v  Local Time Step          1e-006       0.0029893     7.4325e-005      0.00020289

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.61
v  Yplus               0          2.9365         0.62736          0.4825


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51508          2.1317          1.2117          1.1628


 INSTANT    0.928000000E-02   TIME STEP NUMBER             928
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925299E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81082E-02 0.46851E+01
   Friction velocity        uk    :  0.81081E-02 0.46811E+01
   Dimensionless distance   yplus :  0.54975E-02 0.29364E+01
   Friction thermal sca.    tstar :  0.12121E+01 0.31916E+03
   Rough dim-less th. sca.  tplus :  0.38944E-02 0.20802E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26902E+00      10   0.17374E-04   0.62008E+01 0.40241E+02 
c  Velocity[X]                                      0.27207E+01 
c  Velocity[Y]                                      0.15427E+01 
c  Velocity[Z]                                      0.19373E+01 
c  Pressure     0.20313E-04      20   0.36674E-03   0.20937E-01 0.52999E+02 
c  k            0.20956E-01      12   0.75139E-04   0.16753E+00 0.55927E+02 
c  omega        0.27922E+07       1   0.10620E-06   0.22650E+08 0.77462E+00 
c  TempK        0.10042E+05       4   0.47905E-05   0.54454E+01 0.83642E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5319e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.262          19.158       0.0008606       -0.013287
v  Velocity[Y]             -15.193          15.107         0.32415         0.47768
v  Velocity[Z]             -25.202          12.131         -1.6364         -0.5059
v  ǁVelocityǁ         0.00027859          25.612          7.6246          6.5065
v  Pressure                -550.99          179.09          4.2546          9.7604
v  k                   9.7408e-011          10.294         0.25309         0.54935
v  omega                      57.5     2.7319e+008     1.2912e+006           76844
v  TempK                    298.62          363.17          338.21          347.31
v  TurbVisc            2.4411e-018       0.0019766     6.5367e-005      0.00022904
v  CourantNb            0.00022561          1.5309         0.78783         0.96911
v  FourierNb             0.0037991               1         0.42386         0.19378
v  total_pressure      1.0077e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006       0.0030239     7.4328e-005      0.00020289

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.61
v  Yplus               0          2.9364         0.62735         0.48249


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43356          2.1313          1.2117          1.1629


 INSTANT    0.929000000E-02   TIME STEP NUMBER             929
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925228E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81744E-02 0.46854E+01
   Friction velocity        uk    :  0.81744E-02 0.46814E+01
   Dimensionless distance   yplus :  0.55424E-02 0.29362E+01
   Friction thermal sca.    tstar :  0.12120E+01 0.31657E+03
   Rough dim-less th. sca.  tplus :  0.39263E-02 0.20800E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26900E+00      10   0.17455E-04   0.62027E+01 0.40203E+02 
c  Velocity[X]                                      0.27130E+01 
c  Velocity[Y]                                      0.15451E+01 
c  Velocity[Z]                                      0.19446E+01 
c  Pressure     0.20113E-04      19   0.37438E-03   0.20737E-01 0.52048E+02 
c  k            0.20967E-01      12   0.76819E-04   0.17086E+00 0.56319E+02 
c  omega        0.27922E+07       1   0.10343E-06   0.16338E+08 0.68041E+00 
c  TempK        0.10042E+05       4   0.47869E-05   0.54400E+01 0.83605E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.535e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.264          19.156       0.0009046       -0.013315
v  Velocity[Y]             -15.176          15.104          0.3247         0.47855
v  Velocity[Z]             -25.204          12.066         -1.6364        -0.50588
v  ǁVelocityǁ         0.00029495          25.613          7.6243          6.5062
v  Pressure                -550.39          178.79          3.9663          9.4758
v  k                   9.7402e-011          10.076         0.25323         0.54968
v  omega                      57.5     2.7319e+008     1.2912e+006           76843
v  TempK                    298.62          363.17          338.21          347.31
v  TurbVisc            2.4409e-018       0.0019924     6.5411e-005      0.00022921
v  CourantNb             0.0002022          1.5302         0.78782         0.96909
v  FourierNb              0.003799               1          0.4239         0.19388
v  total_pressure      1.0077e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006       0.0030556     7.4332e-005       0.0002029

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.61
v  Yplus               0          2.9362         0.62733         0.48247


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42169          2.1307          1.2117           1.163


 INSTANT    0.930000000E-02   TIME STEP NUMBER             930
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925289E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83152E-02 0.46858E+01
   Friction velocity        uk    :  0.83152E-02 0.46818E+01
   Dimensionless distance   yplus :  0.56379E-02 0.29361E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.31122E+03
   Rough dim-less th. sca.  tplus :  0.39939E-02 0.20799E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26898E+00      10   0.17632E-04   0.62031E+01 0.40150E+02 
c  Velocity[X]                                      0.27058E+01 
c  Velocity[Y]                                      0.15443E+01 
c  Velocity[Z]                                      0.19530E+01 
c  Pressure     0.20107E-04      20   0.38158E-03   0.20738E-01 0.51859E+02 
c  k            0.20977E-01      12   0.78421E-04   0.17429E+00 0.56730E+02 
c  omega        0.27922E+07       1   0.10230E-06   0.12960E+08 0.62116E+00 
c  TempK        0.10042E+05       4   0.47831E-05   0.54370E+01 0.83567E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5383e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.267          19.154      0.00095221       -0.013345
v  Velocity[Y]             -15.092          15.102         0.32524         0.47943
v  Velocity[Z]             -25.205          12.002         -1.6364        -0.50586
v  ǁVelocityǁ         0.00031349          25.615          7.6239          6.5058
v  Pressure                -549.78           178.5          3.6792          9.1925
v  k                   9.7396e-011          10.132         0.25337         0.55001
v  omega                      57.5     2.7319e+008     1.2912e+006           76843
v  TempK                    298.62          363.17          338.22          347.32
v  TurbVisc            2.4408e-018       0.0020074     6.5453e-005      0.00022937
v  CourantNb            0.00017182          1.5295         0.78782         0.96908
v  FourierNb             0.0037989               1         0.42394         0.19398
v  total_pressure      1.0078e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006       0.0030863     7.4335e-005       0.0002029

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.61
v  Yplus               0          2.9361         0.62732         0.48246


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50875          2.1301          1.2118          1.1631


 INSTANT    0.931000000E-02   TIME STEP NUMBER             931
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925208E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84278E-02 0.46861E+01
   Friction velocity        uk    :  0.84278E-02 0.46821E+01
   Dimensionless distance   yplus :  0.57142E-02 0.29359E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.30706E+03
   Rough dim-less th. sca.  tplus :  0.40480E-02 0.20798E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         56 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26896E+00      11   0.17044E-04   0.62114E+01 0.40124E+02 
c  Velocity[X]                                      0.27003E+01 
c  Velocity[Y]                                      0.15459E+01 
c  Velocity[Z]                                      0.19652E+01 
c  Pressure     0.20158E-04      19   0.38472E-03   0.20797E-01 0.50184E+02 
c  k            0.20987E-01      12   0.80603E-04   0.17783E+00 0.57176E+02 
c  omega        0.27922E+07       1   0.10099E-06   0.92694E+07 0.55085E+00 
c  TempK        0.10042E+05       4   0.47799E-05   0.54355E+01 0.83529E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5414e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.269          19.152        0.001001       -0.013376
v  Velocity[Y]             -15.051            15.1         0.32578         0.48032
v  Velocity[Z]             -25.207          11.942         -1.6364        -0.50584
v  ǁVelocityǁ         0.00033192          25.617          7.6235          6.5055
v  Pressure                -549.13          178.21          3.4023          8.9195
v  k                    9.739e-011          10.417         0.25351         0.55034
v  omega                      57.5     2.7319e+008     1.2912e+006           76843
v  TempK                    298.62          363.17          338.22          347.33
v  TurbVisc            2.4406e-018       0.0020275     6.5496e-005      0.00022954
v  CourantNb             0.0001413          1.5287         0.78782         0.96907
v  FourierNb             0.0037988               1         0.42398         0.19409
v  total_pressure      1.0078e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006       0.0031623     7.4339e-005      0.00020291

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.61
v  Yplus               0          2.9359         0.62731         0.48244


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52683          2.1295          1.2118          1.1632


 INSTANT    0.932000000E-02   TIME STEP NUMBER             932
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925283E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.85654E-02 0.46865E+01
   Friction velocity        uk    :  0.85654E-02 0.46825E+01
   Dimensionless distance   yplus :  0.58075E-02 0.29358E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.30213E+03
   Rough dim-less th. sca.  tplus :  0.41140E-02 0.20797E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26894E+00      11   0.17145E-04   0.62133E+01 0.40084E+02 
c  Velocity[X]                                      0.26914E+01 
c  Velocity[Y]                                      0.15476E+01 
c  Velocity[Z]                                      0.19743E+01 
c  Pressure     0.20158E-04      20   0.38475E-03   0.20803E-01 0.50385E+02 
c  k            0.20996E-01      12   0.82469E-04   0.18145E+00 0.57605E+02 
c  omega        0.27922E+07       1   0.10205E-06   0.11557E+08 0.59574E+00 
c  TempK        0.10042E+05       4   0.47777E-05   0.54371E+01 0.83494E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5439e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.272          19.151       0.0010521       -0.013407
v  Velocity[Y]             -15.068          15.098         0.32633         0.48121
v  Velocity[Z]             -25.209          11.884         -1.6364        -0.50582
v  ǁVelocityǁ         0.00035095          25.619          7.6232          6.5051
v  Pressure                -548.45          177.92          3.1236          8.6442
v  k                   9.7384e-011           10.47         0.25365         0.55066
v  omega                      57.5     2.7319e+008     1.2912e+006           76843
v  TempK                    298.62          363.17          338.22          347.34
v  TurbVisc            2.4404e-018       0.0020435     6.5537e-005      0.00022971
v  CourantNb            0.00013496          1.5281         0.78781         0.96906
v  FourierNb             0.0037986               1         0.42402         0.19419
v  total_pressure      1.0078e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006       0.0032078     7.4342e-005      0.00020291

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.61
v  Yplus               0          2.9358          0.6273         0.48242


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64536           2.129          1.2118          1.1632


 INSTANT    0.933000000E-02   TIME STEP NUMBER             933
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925121E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.86853E-02 0.46868E+01
   Friction velocity        uk    :  0.86852E-02 0.46828E+01
   Dimensionless distance   yplus :  0.58887E-02 0.29356E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.29796E+03
   Rough dim-less th. sca.  tplus :  0.41716E-02 0.20796E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26892E+00      11   0.17262E-04   0.62240E+01 0.40078E+02 
c  Velocity[X]                                      0.26866E+01 
c  Velocity[Y]                                      0.15528E+01 
c  Velocity[Z]                                      0.19845E+01 
c  Pressure     0.20462E-04      19   0.38038E-03   0.21123E-01 0.46757E+02 
c  k            0.21006E-01      12   0.83446E-04   0.18530E+00 0.58075E+02 
c  omega        0.27922E+07       1   0.10518E-06   0.18968E+08 0.72069E+00 
c  TempK        0.10042E+05       4   0.47755E-05   0.54362E+01 0.83433E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.546e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.274          19.149       0.0011051       -0.013439
v  Velocity[Y]             -15.158          15.096         0.32687         0.48211
v  Velocity[Z]             -25.211           11.83         -1.6364         -0.5058
v  ǁVelocityǁ         0.00037283           25.62          7.6228          6.5048
v  Pressure                -547.76          177.66          2.8688          8.3924
v  k                   9.7378e-011           10.44         0.25378         0.55098
v  omega                      57.5     2.7319e+008     1.2912e+006           76843
v  TempK                    298.62          363.17          338.23          347.34
v  TurbVisc            2.4403e-018       0.0020495     6.5577e-005      0.00022987
v  CourantNb            0.00013819          1.5277         0.78781         0.96904
v  FourierNb             0.0037985               1         0.42406         0.19429
v  total_pressure      1.0078e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006       0.0031596     7.4346e-005      0.00020292

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.61
v  Yplus               0          2.9356         0.62729         0.48241


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52456          2.1287          1.2119          1.1633


 INSTANT    0.934000000E-02   TIME STEP NUMBER             934
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925268E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88693E-02 0.46871E+01
   Friction velocity        uk    :  0.88693E-02 0.46831E+01
   Dimensionless distance   yplus :  0.60136E-02 0.29354E+01
   Friction thermal sca.    tstar :  0.12119E+01 0.29178E+03
   Rough dim-less th. sca.  tplus :  0.42600E-02 0.20794E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26891E+00      11   0.17343E-04   0.62274E+01 0.40042E+02 
c  Velocity[X]                                      0.26805E+01 
c  Velocity[Y]                                      0.15549E+01 
c  Velocity[Z]                                      0.19920E+01 
c  Pressure     0.20329E-04      19   0.37804E-03   0.20991E-01 0.48620E+02 
c  k            0.21015E-01      12   0.84917E-04   0.18901E+00 0.58523E+02 
c  omega        0.27922E+07       1   0.10621E-06   0.22518E+08 0.77379E+00 
c  TempK        0.10042E+05       4   0.47735E-05   0.54284E+01 0.83347E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5479e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.276          19.148       0.0011605       -0.013471
v  Velocity[Y]             -15.214          15.094          0.3274         0.48301
v  Velocity[Z]             -25.212          11.779         -1.6364        -0.50579
v  ǁVelocityǁ          0.0003925          25.622          7.6224          6.5044
v  Pressure                -547.06          177.38          2.6011          8.1277
v  k                   9.7372e-011          10.257         0.25391         0.55129
v  omega                      57.5     2.7319e+008     1.2912e+006           76843
v  TempK                    298.62          363.17          338.23          347.35
v  TurbVisc            2.4401e-018       0.0020617     6.5616e-005      0.00023003
v  CourantNb            0.00014154          1.5272          0.7878         0.96903
v  FourierNb             0.0037983               1          0.4241         0.19439
v  total_pressure      1.0078e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034741     7.4349e-005      0.00020293

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.61
v  Yplus               0          2.9354         0.62728          0.4824


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54206          2.1284          1.2119          1.1634


 INSTANT    0.935000000E-02   TIME STEP NUMBER             935
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925228E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89288E-02 0.46875E+01
   Friction velocity        uk    :  0.89288E-02 0.46835E+01
   Dimensionless distance   yplus :  0.60539E-02 0.29351E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.28984E+03
   Rough dim-less th. sca.  tplus :  0.42886E-02 0.20793E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26889E+00      11   0.17423E-04   0.62222E+01 0.39976E+02 
c  Velocity[X]                                      0.26714E+01 
c  Velocity[Y]                                      0.15551E+01 
c  Velocity[Z]                                      0.19957E+01 
c  Pressure     0.19919E-04      19   0.37230E-03   0.20572E-01 0.47140E+02 
c  k            0.21024E-01      12   0.86214E-04   0.19247E+00 0.58920E+02 
c  omega        0.27922E+07       1   0.10419E-06   0.16754E+08 0.68803E+00 
c  TempK        0.10042E+05       4   0.47721E-05   0.54187E+01 0.83235E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5506e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.278          19.146       0.0012147       -0.013502
v  Velocity[Y]             -15.153          15.093         0.32793         0.48392
v  Velocity[Z]             -25.214          11.754         -1.6364        -0.50578
v  ǁVelocityǁ         0.00041328          25.624           7.622          6.5041
v  Pressure                -546.36          177.11           2.342          7.8722
v  k                   9.7366e-011          10.177         0.25403          0.5516
v  omega                      57.5     2.7319e+008     1.2912e+006           76843
v  TempK                    298.62          363.17          338.23          347.36
v  TurbVisc              2.44e-018       0.0020628     6.5654e-005      0.00023018
v  CourantNb             0.0001448          1.5266          0.7878         0.96902
v  FourierNb             0.0037981               1         0.42414         0.19449
v  total_pressure      1.0078e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006       0.0038215     7.4354e-005      0.00020294

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.61
v  Yplus               0          2.9351         0.62727         0.48239


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54877          2.1279          1.2119          1.1635


 INSTANT    0.936000000E-02   TIME STEP NUMBER             936
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925183E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.90395E-02 0.46878E+01
   Friction velocity        uk    :  0.90395E-02 0.46838E+01
   Dimensionless distance   yplus :  0.61289E-02 0.29349E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.28629E+03
   Rough dim-less th. sca.  tplus :  0.43418E-02 0.20791E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26887E+00      11   0.17531E-04   0.62095E+01 0.39878E+02 
c  Velocity[X]                                      0.26611E+01 
c  Velocity[Y]                                      0.15500E+01 
c  Velocity[Z]                                      0.19984E+01 
c  Pressure     0.19830E-04      20   0.36492E-03   0.20486E-01 0.45778E+02 
c  k            0.21032E-01      12   0.87002E-04   0.19605E+00 0.59321E+02 
c  omega        0.27922E+07       1   0.10217E-06   0.99496E+07 0.56686E+00 
c  TempK        0.10042E+05       4   0.47695E-05   0.54125E+01 0.83140E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5534e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.28          19.145       0.0012712        -0.01353
v  Velocity[Y]             -15.095          15.092         0.32846         0.48483
v  Velocity[Z]             -25.216          11.996         -1.6365        -0.50577
v  ǁVelocityǁ         0.00042729          25.626          7.6217          6.5037
v  Pressure                -545.66          176.86          2.0918          7.6256
v  k                   9.7361e-011          10.265         0.25416          0.5519
v  omega                      57.5     2.7319e+008     1.2912e+006           76843
v  TempK                    298.62          363.17          338.24          347.37
v  TurbVisc            2.4399e-018       0.0020634     6.5691e-005      0.00023034
v  CourantNb            0.00016647          1.5259         0.78779           0.969
v  FourierNb              0.003798               1         0.42418         0.19459
v  total_pressure      1.0078e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006       0.0042037     7.4358e-005      0.00020295

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.61
v  Yplus               0          2.9349         0.62726         0.48238


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39682          2.1274           1.212          1.1636


 INSTANT    0.937000000E-02   TIME STEP NUMBER             937
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925234E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91285E-02 0.46881E+01
   Friction velocity        uk    :  0.91285E-02 0.46841E+01
   Dimensionless distance   yplus :  0.61893E-02 0.29347E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.28350E+03
   Rough dim-less th. sca.  tplus :  0.43845E-02 0.20790E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         54 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26886E+00      11   0.17662E-04   0.62046E+01 0.39812E+02 
c  Velocity[X]                                      0.26518E+01 
c  Velocity[Y]                                      0.15503E+01 
c  Velocity[Z]                                      0.20024E+01 
c  Pressure     0.19585E-04      19   0.36429E-03   0.20238E-01 0.44370E+02 
c  k            0.21041E-01      12   0.88193E-04   0.19979E+00 0.59725E+02 
c  omega        0.27922E+07       1   0.10195E-06   0.96584E+07 0.56173E+00 
c  TempK        0.10041E+05       4   0.47660E-05   0.54039E+01 0.83031E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5559e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.282          19.144       0.0013297       -0.013557
v  Velocity[Y]              -15.08          15.091         0.32898         0.48575
v  Velocity[Z]             -25.218          12.273         -1.6365        -0.50576
v  ǁVelocityǁ         0.00042678          25.628          7.6213          6.5034
v  Pressure                -544.96           176.6          1.8493          7.3864
v  k                   9.7355e-011          10.342         0.25428         0.55219
v  omega                      57.5     2.7319e+008     1.2912e+006           76842
v  TempK                    298.62          363.17          338.24          347.37
v  TurbVisc            2.4397e-018       0.0020639     6.5727e-005      0.00023049
v  CourantNb            0.00016601          1.5253         0.78778         0.96899
v  FourierNb             0.0037978               1         0.42422         0.19469
v  total_pressure      1.0078e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006        0.004624     7.4363e-005      0.00020296

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.61
v  Yplus               0          2.9347         0.62725         0.48236


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41164           2.127           1.212          1.1637


 INSTANT    0.938000000E-02   TIME STEP NUMBER             938
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925186E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92343E-02 0.46884E+01
   Friction velocity        uk    :  0.92343E-02 0.46844E+01
   Dimensionless distance   yplus :  0.62610E-02 0.29345E+01
   Friction thermal sca.    tstar :  0.12115E+01 0.28026E+03
   Rough dim-less th. sca.  tplus :  0.44353E-02 0.20788E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26884E+00      11   0.17772E-04   0.62040E+01 0.39757E+02 
c  Velocity[X]                                      0.26435E+01 
c  Velocity[Y]                                      0.15515E+01 
c  Velocity[Z]                                      0.20090E+01 
c  Pressure     0.19974E-04      19   0.36638E-03   0.20646E-01 0.42558E+02 
c  k            0.21049E-01      12   0.89366E-04   0.20358E+00 0.60102E+02 
c  omega        0.27922E+07       1   0.10250E-06   0.12543E+08 0.60909E+00 
c  TempK        0.10041E+05       4   0.47627E-05   0.53998E+01 0.82940E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5579e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.284          19.142       0.0013908       -0.013581
v  Velocity[Y]             -15.136           15.09          0.3295         0.48667
v  Velocity[Z]              -25.22          11.746         -1.6365        -0.50576
v  ǁVelocityǁ         0.00042627           25.63           7.621           6.503
v  Pressure                -544.25          176.37          1.6187          7.1588
v  k                    9.735e-011          10.373          0.2544         0.55248
v  omega                      57.5     2.7319e+008     1.2912e+006           76842
v  TempK                    298.61          363.17          338.25          347.38
v  TurbVisc            2.4396e-018       0.0020646     6.5763e-005      0.00023063
v  CourantNb             0.0001662          1.5249         0.78778         0.96898
v  FourierNb             0.0037976               1         0.42426         0.19478
v  total_pressure      1.0078e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006       0.0050864     7.4368e-005      0.00020297

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.62
v  Yplus               0          2.9345         0.62724         0.48235


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.2697          2.1266           1.212          1.1638


 INSTANT    0.939000000E-02   TIME STEP NUMBER             939
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925240E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93337E-02 0.46887E+01
   Friction velocity        uk    :  0.93337E-02 0.46847E+01
   Dimensionless distance   yplus :  0.63284E-02 0.29342E+01
   Friction thermal sca.    tstar :  0.12115E+01 0.27727E+03
   Rough dim-less th. sca.  tplus :  0.44831E-02 0.20786E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26883E+00      11   0.17841E-04   0.62129E+01 0.39753E+02 
c  Velocity[X]                                      0.26369E+01 
c  Velocity[Y]                                      0.15591E+01 
c  Velocity[Z]                                      0.20169E+01 
c  Pressure     0.19854E-04      19   0.37619E-03   0.20526E-01 0.41077E+02 
c  k            0.21056E-01      12   0.90903E-04   0.20773E+00 0.60517E+02 
c  omega        0.27922E+07       1   0.10590E-06   0.21843E+08 0.75210E+00 
c  TempK        0.10041E+05       4   0.47595E-05   0.53969E+01 0.82863E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5595e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.285          19.141       0.0014537       -0.013605
v  Velocity[Y]             -15.199          15.089         0.33002         0.48759
v  Velocity[Z]             -25.222          12.231         -1.6366        -0.50575
v  ǁVelocityǁ         0.00042553          25.632          7.6206          6.5027
v  Pressure                -543.54          176.14          1.3976          6.9398
v  k                   9.7345e-011          10.261         0.25451         0.55276
v  omega                      57.5     2.7319e+008     1.2912e+006           76842
v  TempK                    298.61          363.17          338.25          347.39
v  TurbVisc            2.4394e-018       0.0020653     6.5797e-005      0.00023077
v  CourantNb            0.00016474          1.5245         0.78777         0.96896
v  FourierNb             0.0037975               1         0.42429         0.19487
v  total_pressure      1.0078e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006       0.0050236     7.4372e-005      0.00020298

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.62
v  Yplus               0          2.9342         0.62723         0.48234


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.36069          2.1264          1.2121          1.1638


 INSTANT    0.940000000E-02   TIME STEP NUMBER             940
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925246E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94866E-02 0.46889E+01
   Friction velocity        uk    :  0.94865E-02 0.46849E+01
   Dimensionless distance   yplus :  0.64320E-02 0.29339E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.27281E+03
   Rough dim-less th. sca.  tplus :  0.45565E-02 0.20784E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26881E+00      11   0.17950E-04   0.62204E+01 0.39729E+02 
c  Velocity[X]                                      0.26323E+01 
c  Velocity[Y]                                      0.15644E+01 
c  Velocity[Z]                                      0.20236E+01 
c  Pressure     0.20443E-04      20   0.37508E-03   0.21141E-01 0.41849E+02 
c  k            0.21064E-01      12   0.91620E-04   0.21208E+00 0.60904E+02 
c  omega        0.27922E+07       1   0.10454E-06   0.20336E+08 0.73350E+00 
c  TempK        0.10041E+05       4   0.47561E-05   0.53968E+01 0.82787E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5618e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.287           19.14       0.0015168       -0.013627
v  Velocity[Y]             -15.185          15.089         0.33054         0.48852
v  Velocity[Z]             -25.224          12.226         -1.6366        -0.50574
v  ǁVelocityǁ          0.0004252          25.634          7.6202          6.5024
v  Pressure                -542.84           175.9          1.1707          6.7155
v  k                    9.734e-011          10.036         0.25462         0.55303
v  omega                      57.5     2.7319e+008     1.2912e+006           76842
v  TempK                     298.6          363.17          338.25          347.39
v  TurbVisc            2.4393e-018       0.0020595      6.583e-005      0.00023091
v  CourantNb            0.00016226           1.524         0.78777         0.96895
v  FourierNb             0.0037973               1         0.42433         0.19496
v  total_pressure      1.0078e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034185     7.4376e-005      0.00020299

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.62
v  Yplus               0          2.9339         0.62722         0.48233


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5321           2.126          1.2121          1.1639


 INSTANT    0.941000000E-02   TIME STEP NUMBER             941
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925124E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95512E-02 0.46892E+01
   Friction velocity        uk    :  0.95512E-02 0.46852E+01
   Dimensionless distance   yplus :  0.64759E-02 0.29336E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.27096E+03
   Rough dim-less th. sca.  tplus :  0.45876E-02 0.20782E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26880E+00      11   0.18046E-04   0.62197E+01 0.39643E+02 
c  Velocity[X]                                      0.26253E+01 
c  Velocity[Y]                                      0.15646E+01 
c  Velocity[Z]                                      0.20298E+01 
c  Pressure     0.20028E-04      20   0.38204E-03   0.20718E-01 0.40751E+02 
c  k            0.21071E-01      12   0.92410E-04   0.21649E+00 0.61279E+02 
c  omega        0.27922E+07       1   0.10405E-06   0.20829E+08 0.73901E+00 
c  TempK        0.10041E+05       4   0.47522E-05   0.53925E+01 0.82656E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5642e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.288          19.139       0.0015817       -0.013648
v  Velocity[Y]             -15.111          15.089         0.33106         0.48945
v  Velocity[Z]             -25.226          12.819         -1.6366        -0.50573
v  ǁVelocityǁ         0.00042482          25.636          7.6199          6.5021
v  Pressure                -542.15          175.68         0.95047          6.4984
v  k                   9.7335e-011          10.038         0.25473         0.55329
v  omega                      57.5     2.7319e+008     1.2912e+006           76842
v  TempK                     298.6          363.17          338.26           347.4
v  TurbVisc            2.4392e-018       0.0020511     6.5862e-005      0.00023105
v  CourantNb            0.00015509          1.5234         0.78776         0.96894
v  FourierNb             0.0037971               1         0.42436         0.19505
v  total_pressure      1.0078e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034509     7.4381e-005        0.000203

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.62
v  Yplus               0          2.9336         0.62721         0.48231


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55441          2.1256          1.2121           1.164


 INSTANT    0.942000000E-02   TIME STEP NUMBER             942
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925118E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96264E-02 0.46895E+01
   Friction velocity        uk    :  0.96264E-02 0.46855E+01
   Dimensionless distance   yplus :  0.65269E-02 0.29333E+01
   Friction thermal sca.    tstar :  0.12113E+01 0.26885E+03
   Rough dim-less th. sca.  tplus :  0.46237E-02 0.20780E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         55 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26878E+00      11   0.18151E-04   0.62236E+01 0.39571E+02 
c  Velocity[X]                                      0.26225E+01 
c  Velocity[Y]                                      0.15658E+01 
c  Velocity[Z]                                      0.20353E+01 
c  Pressure     0.20682E-04      19   0.38415E-03   0.21402E-01 0.39000E+02 
c  k            0.21078E-01      12   0.93865E-04   0.22082E+00 0.61656E+02 
c  omega        0.27922E+07       1   0.10017E-06   0.90314E+07 0.52927E+00 
c  TempK        0.10041E+05       4   0.47492E-05   0.53975E+01 0.82575E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5664e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.29          19.138       0.0016468       -0.013669
v  Velocity[Y]             -15.076          15.089         0.33157         0.49038
v  Velocity[Z]             -25.229          11.738         -1.6367        -0.50573
v  ǁVelocityǁ         0.00042446          25.638          7.6195          6.5018
v  Pressure                -541.46          175.46          0.7411          6.2919
v  k                   9.7331e-011          10.288         0.25484         0.55354
v  omega                      57.5     2.7319e+008     1.2912e+006           76842
v  TempK                     298.6          363.17          338.26          347.41
v  TurbVisc            2.4391e-018       0.0020489     6.5892e-005      0.00023117
v  CourantNb            0.00014746          1.5229         0.78776         0.96893
v  FourierNb             0.0037969               1          0.4244         0.19513
v  total_pressure      1.0078e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006        0.003631     7.4384e-005      0.00020301

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.62
v  Yplus               0          2.9333         0.62719          0.4823


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56816          2.1253          1.2122          1.1641


 INSTANT    0.943000000E-02   TIME STEP NUMBER             943
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925220E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96947E-02 0.46897E+01
   Friction velocity        uk    :  0.96947E-02 0.46857E+01
   Dimensionless distance   yplus :  0.65732E-02 0.29330E+01
   Friction thermal sca.    tstar :  0.12113E+01 0.26696E+03
   Rough dim-less th. sca.  tplus :  0.46565E-02 0.20778E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         54 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26877E+00      11   0.18240E-04   0.62342E+01 0.39529E+02 
c  Velocity[X]                                      0.26198E+01 
c  Velocity[Y]                                      0.15709E+01 
c  Velocity[Z]                                      0.20435E+01 
c  Pressure     0.20292E-04      19   0.41551E-03   0.21005E-01 0.38575E+02 
c  k            0.21084E-01      12   0.94371E-04   0.22488E+00 0.61957E+02 
c  omega        0.27922E+07       1   0.99799E-07   0.85635E+07 0.52197E+00 
c  TempK        0.10041E+05       4   0.47467E-05   0.53886E+01 0.82482E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5679e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.291          19.137       0.0017106        -0.01369
v  Velocity[Y]             -15.098           15.09         0.33209         0.49131
v  Velocity[Z]             -25.231          11.739         -1.6367        -0.50573
v  ǁVelocityǁ         0.00042404           25.64          7.6192          6.5015
v  Pressure                -540.77          175.25         0.53377          6.0872
v  k                   9.7326e-011          10.371         0.25494         0.55378
v  omega                      57.5     2.7319e+008     1.2912e+006           76842
v  TempK                     298.6          363.17          338.26          347.42
v  TurbVisc             2.439e-018       0.0020497     6.5922e-005       0.0002313
v  CourantNb            0.00014046          1.5225         0.78776         0.96893
v  FourierNb             0.0037967               1         0.42443         0.19521
v  total_pressure      1.0078e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006       0.0037582     7.4389e-005      0.00020302

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.62
v  Yplus               0           2.933         0.62718         0.48229


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51736          2.1251          1.2122          1.1641


 INSTANT    0.944000000E-02   TIME STEP NUMBER             944
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925114E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97816E-02 0.46900E+01
   Friction velocity        uk    :  0.97815E-02 0.46860E+01
   Dimensionless distance   yplus :  0.66320E-02 0.29327E+01
   Friction thermal sca.    tstar :  0.12113E+01 0.26459E+03
   Rough dim-less th. sca.  tplus :  0.46982E-02 0.20775E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26876E+00      11   0.18335E-04   0.62501E+01 0.39504E+02 
c  Velocity[X]                                      0.26197E+01 
c  Velocity[Y]                                      0.15775E+01 
c  Velocity[Z]                                      0.20529E+01 
c  Pressure     0.20828E-04      19   0.38140E-03   0.21569E-01 0.35839E+02 
c  k            0.21090E-01      13   0.93604E-04   0.22891E+00 0.62278E+02 
c  omega        0.27922E+07       1   0.10086E-06   0.11554E+08 0.58112E+00 
c  TempK        0.10041E+05       4   0.47439E-05   0.53783E+01 0.82373E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.569e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.292          19.136       0.0017723       -0.013709
v  Velocity[Y]              -15.19           15.09         0.33261         0.49225
v  Velocity[Z]             -25.233           11.74         -1.6368        -0.50572
v  ǁVelocityǁ         0.00042377          25.643          7.6188          6.5012
v  Pressure                -540.06          175.06         0.34395             5.9
v  k                   9.7322e-011          10.361         0.25504         0.55402
v  omega                      57.5      2.732e+008     1.2912e+006           76842
v  TempK                    298.59          363.17          338.27          347.42
v  TurbVisc            2.4388e-018       0.0020505      6.595e-005      0.00023142
v  CourantNb            0.00013429          1.5223         0.78777         0.96894
v  FourierNb             0.0037965               1         0.42446         0.19529
v  total_pressure      1.0078e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006       0.0036055     7.4392e-005      0.00020304

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.62
v  Yplus               0          2.9327         0.62718         0.48227


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4883           2.125          1.2122          1.1642


 INSTANT    0.945000000E-02   TIME STEP NUMBER             945
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925196E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98316E-02 0.46902E+01
   Friction velocity        uk    :  0.98316E-02 0.46862E+01
   Dimensionless distance   yplus :  0.66660E-02 0.29324E+01
   Friction thermal sca.    tstar :  0.12112E+01 0.30920E+03
   Rough dim-less th. sca.  tplus :  0.47222E-02 0.20773E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26874E+00      11   0.18431E-04   0.62672E+01 0.39507E+02 
c  Velocity[X]                                      0.26175E+01 
c  Velocity[Y]                                      0.15866E+01 
c  Velocity[Z]                                      0.20631E+01 
c  Pressure     0.20052E-04      20   0.37786E-03   0.20773E-01 0.35114E+02 
c  k            0.21096E-01      13   0.93963E-04   0.23248E+00 0.62553E+02 
c  omega        0.27922E+07       1   0.10280E-06   0.17607E+08 0.68549E+00 
c  TempK        0.10041E+05       4   0.47422E-05   0.53750E+01 0.82287E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5698e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.293          19.135       0.0018337       -0.013727
v  Velocity[Y]             -15.251          15.091         0.33312         0.49319
v  Velocity[Z]             -25.236          12.139         -1.6369        -0.50572
v  ǁVelocityǁ         0.00042324          25.645          7.6185          6.5009
v  Pressure                -539.35          174.87         0.15882          5.7167
v  k                   9.7317e-011          10.143         0.25514         0.55424
v  omega                    57.501      2.732e+008     1.2912e+006           76842
v  TempK                    298.59          363.17          338.27          347.43
v  TurbVisc            2.4387e-018       0.0020513     6.5977e-005      0.00023154
v  CourantNb            0.00012686          1.5221         0.78776         0.96894
v  FourierNb             0.0037963               1         0.42449         0.19536
v  total_pressure      1.0079e+005      1.015e+005     1.0133e+005     1.0133e+005
v  Local Time Step          1e-006       0.0037256     7.4394e-005      0.00020305

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.62
v  Yplus               0          2.9324         0.62717         0.48226


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51122          2.1249          1.2122          1.1643


 INSTANT    0.946000000E-02   TIME STEP NUMBER             946
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925171E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99359E-02 0.46905E+01
   Friction velocity        uk    :  0.99359E-02 0.46864E+01
   Dimensionless distance   yplus :  0.67367E-02 0.29320E+01
   Friction thermal sca.    tstar :  0.12113E+01 0.26048E+03
   Rough dim-less th. sca.  tplus :  0.47723E-02 0.20771E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26873E+00      11   0.18516E-04   0.62874E+01 0.39532E+02 
c  Velocity[X]                                      0.26182E+01 
c  Velocity[Y]                                      0.16005E+01 
c  Velocity[Z]                                      0.20688E+01 
c  Pressure     0.20432E-04      19   0.37278E-03   0.21174E-01 0.33962E+02 
c  k            0.21102E-01      13   0.94754E-04   0.23574E+00 0.62778E+02 
c  omega        0.27922E+07       1   0.10419E-06   0.21921E+08 0.75443E+00 
c  TempK        0.10041E+05       4   0.47417E-05   0.53612E+01 0.82143E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5713e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.293          19.135       0.0018964       -0.013742
v  Velocity[Y]             -15.188          15.092         0.33364         0.49413
v  Velocity[Z]             -25.238          11.741         -1.6369        -0.50572
v  ǁVelocityǁ         0.00042275          25.647          7.6182          6.5007
v  Pressure                -538.63          174.68       -0.019507          5.5404
v  k                   9.7313e-011          9.9577         0.25524         0.55446
v  omega                    57.501      2.732e+008     1.2912e+006           76841
v  TempK                    298.59          363.17          338.28          347.44
v  TurbVisc            2.4386e-018       0.0020521     6.6003e-005      0.00023165
v  CourantNb            0.00011898          1.5218         0.78776         0.96894
v  FourierNb             0.0037961               1         0.42451         0.19544
v  total_pressure      1.0079e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0040981     7.4397e-005      0.00020306

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.62
v  Yplus               0           2.932         0.62716         0.48225


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45327          2.1247          1.2123          1.1644


 INSTANT    0.947000000E-02   TIME STEP NUMBER             947
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925205E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10030E-01 0.46907E+01
   Friction velocity        uk    :  0.10030E-01 0.46867E+01
   Dimensionless distance   yplus :  0.68004E-02 0.29317E+01
   Friction thermal sca.    tstar :  0.12114E+01 0.25804E+03
   Rough dim-less th. sca.  tplus :  0.48175E-02 0.20768E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26872E+00      11   0.18597E-04   0.62925E+01 0.39466E+02 
c  Velocity[X]                                      0.26171E+01 
c  Velocity[Y]                                      0.16025E+01 
c  Velocity[Z]                                      0.20730E+01 
c  Pressure     0.20183E-04      19   0.37808E-03   0.20925E-01 0.34859E+02 
c  k            0.21106E-01      13   0.95434E-04   0.23879E+00 0.62995E+02 
c  omega        0.27922E+07       1   0.10149E-06   0.14881E+08 0.64601E+00 
c  TempK        0.10041E+05       4   0.47416E-05   0.53494E+01 0.81998E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5729e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.294          19.134       0.0019576       -0.013754
v  Velocity[Y]             -15.129          15.093         0.33416         0.49506
v  Velocity[Z]              -25.24          12.609          -1.637        -0.50572
v  ǁVelocityǁ         0.00042262          25.649          7.6178          6.5004
v  Pressure                -537.92          174.49        -0.20411          5.3584
v  k                    9.731e-011          9.8988         0.25533         0.55466
v  omega                    57.501      2.732e+008     1.2912e+006           76841
v  TempK                    298.59          363.17          338.28          347.44
v  TurbVisc            2.4385e-018       0.0020528     6.6028e-005      0.00023176
v  CourantNb            0.00011068          1.5214         0.78776         0.96894
v  FourierNb             0.0037959               1         0.42454         0.19551
v  total_pressure      1.0079e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0039892     7.4399e-005      0.00020307

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.62
v  Yplus               0          2.9317         0.62715         0.48223


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46764          2.1245          1.2123          1.1644


 INSTANT    0.948000000E-02   TIME STEP NUMBER             948
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925132E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10063E-01 0.46909E+01
   Friction velocity        uk    :  0.10063E-01 0.46869E+01
   Dimensionless distance   yplus :  0.68229E-02 0.29313E+01
   Friction thermal sca.    tstar :  0.12111E+01 0.25719E+03
   Rough dim-less th. sca.  tplus :  0.48334E-02 0.20765E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         54 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26871E+00      11   0.18684E-04   0.63013E+01 0.39418E+02 
c  Velocity[X]                                      0.26158E+01 
c  Velocity[Y]                                      0.16067E+01 
c  Velocity[Z]                                      0.20787E+01 
c  Pressure     0.20486E-04      19   0.37722E-03   0.21248E-01 0.33872E+02 
c  k            0.21111E-01      13   0.96176E-04   0.24156E+00 0.63171E+02 
c  omega        0.27922E+07       1   0.99051E-07   0.88860E+07 0.53489E+00 
c  TempK        0.10041E+05       4   0.47404E-05   0.53378E+01 0.81866E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5741e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.295          19.133       0.0020211        -0.01376
v  Velocity[Y]             -15.115          15.095         0.33468           0.496
v  Velocity[Z]             -25.243          11.739          -1.637        -0.50572
v  ǁVelocityǁ         0.00042233          25.651          7.6175          6.5002
v  Pressure                 -537.2          174.31         -0.3816          5.1833
v  k                   9.7306e-011          9.9661         0.25542         0.55485
v  omega                    57.501      2.732e+008     1.2912e+006           76841
v  TempK                    298.59          363.17          338.28          347.45
v  TurbVisc            2.4384e-018        0.002061     6.6053e-005      0.00023187
v  CourantNb              0.000102          1.5211         0.78776         0.96894
v  FourierNb             0.0037957               1         0.42457         0.19558
v  total_pressure      1.0079e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0032051     7.4399e-005      0.00020309

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.62
v  Yplus               0          2.9313         0.62714         0.48222


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.30197          2.1244          1.2123          1.1645


 INSTANT    0.949000000E-02   TIME STEP NUMBER             949
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925108E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10113E-01 0.46911E+01
   Friction velocity        uk    :  0.10113E-01 0.46871E+01
   Dimensionless distance   yplus :  0.68569E-02 0.29309E+01
   Friction thermal sca.    tstar :  0.12110E+01 0.25592E+03
   Rough dim-less th. sca.  tplus :  0.48575E-02 0.20763E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26870E+00      11   0.18787E-04   0.63144E+01 0.39397E+02 
c  Velocity[X]                                      0.26151E+01 
c  Velocity[Y]                                      0.16143E+01 
c  Velocity[Z]                                      0.20849E+01 
c  Pressure     0.20589E-04      19   0.37371E-03   0.21363E-01 0.31580E+02 
c  k            0.21116E-01      13   0.95996E-04   0.24402E+00 0.63328E+02 
c  omega        0.27922E+07       1   0.98794E-07   0.80894E+07 0.51777E+00 
c  TempK        0.10041E+05       4   0.47399E-05   0.53290E+01 0.81740E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5748e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.295          19.132       0.0020876       -0.013763
v  Velocity[Y]             -15.133          15.097          0.3352         0.49694
v  Velocity[Z]             -25.245          11.737         -1.6371        -0.50572
v  ǁVelocityǁ         0.00042195          25.654          7.6172             6.5
v  Pressure                -536.48          174.14        -0.54559          5.0217
v  k                   9.7302e-011          9.9439          0.2555         0.55503
v  omega                    57.501      2.732e+008     1.2912e+006           76841
v  TempK                    298.59          363.17          338.29          347.46
v  TurbVisc            2.4383e-018       0.0020777     6.6076e-005      0.00023197
v  CourantNb           9.2574e-005           1.521         0.78777         0.96895
v  FourierNb             0.0037955               1         0.42459         0.19565
v  total_pressure      1.0079e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034426     7.4399e-005       0.0002031

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.62
v  Yplus               0          2.9309         0.62713         0.48221


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35233          2.1244          1.2124          1.1646


 INSTANT    0.950000000E-02   TIME STEP NUMBER             950
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925156E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10189E-01 0.46912E+01
   Friction velocity        uk    :  0.10189E-01 0.46872E+01
   Dimensionless distance   yplus :  0.69081E-02 0.29305E+01
   Friction thermal sca.    tstar :  0.12109E+01 0.25402E+03
   Rough dim-less th. sca.  tplus :  0.48938E-02 0.20760E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26869E+00      11   0.18916E-04   0.63285E+01 0.39392E+02 
c  Velocity[X]                                      0.26158E+01 
c  Velocity[Y]                                      0.16204E+01 
c  Velocity[Z]                                      0.20923E+01 
c  Pressure     0.20830E-04      19   0.37594E-03   0.21622E-01 0.30321E+02 
c  k            0.21120E-01      13   0.96777E-04   0.24615E+00 0.63474E+02 
c  omega        0.27922E+07       1   0.99737E-07   0.10318E+08 0.56120E+00 
c  TempK        0.10041E+05       4   0.47389E-05   0.53159E+01 0.81603E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5749e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.295          19.132       0.0021592       -0.013759
v  Velocity[Y]             -15.225          15.099         0.33572         0.49787
v  Velocity[Z]             -25.248          11.735         -1.6372        -0.50573
v  ǁVelocityǁ         0.00042183          25.656          7.6169          6.4998
v  Pressure                 -535.7          173.99        -0.70118          4.8679
v  k                   9.7299e-011          9.8387         0.25559         0.55519
v  omega                    57.501      2.732e+008     1.2912e+006           76841
v  TempK                    298.59          363.17          338.29          347.46
v  TurbVisc            2.4383e-018       0.0020939       6.61e-005      0.00023207
v  CourantNb           8.2969e-005          1.5209         0.78777         0.96895
v  FourierNb             0.0037953               1         0.42462         0.19572
v  total_pressure      1.0079e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0036671       7.44e-005      0.00020312

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.62
v  Yplus               0          2.9305         0.62712         0.48219


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57802          2.1245          1.2124          1.1647


 INSTANT    0.951000000E-02   TIME STEP NUMBER             951
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925161E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10214E-01 0.46914E+01
   Friction velocity        uk    :  0.10214E-01 0.46874E+01
   Dimensionless distance   yplus :  0.69250E-02 0.29301E+01
   Friction thermal sca.    tstar :  0.12110E+01 0.25341E+03
   Rough dim-less th. sca.  tplus :  0.49057E-02 0.20757E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26868E+00      11   0.19010E-04   0.63406E+01 0.39391E+02 
c  Velocity[X]                                      0.26167E+01 
c  Velocity[Y]                                      0.16277E+01 
c  Velocity[Z]                                      0.20962E+01 
c  Pressure     0.21203E-04      23   0.37574E-03   0.22018E-01 0.29185E+02 
c  k            0.21124E-01      13   0.96417E-04   0.24782E+00 0.63564E+02 
c  omega        0.27922E+07       1   0.10398E-06   0.24614E+08 0.79409E+00 
c  TempK        0.10041E+05       4   0.47377E-05   0.53108E+01 0.81501E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.575e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.295          19.131       0.0022343       -0.013752
v  Velocity[Y]             -15.271          15.101         0.33623          0.4988
v  Velocity[Z]              -25.25          12.918         -1.6373        -0.50573
v  ǁVelocityǁ         0.00042143          25.659          7.6166          6.4996
v  Pressure                -534.88          173.83        -0.85008          4.7206
v  k                   9.7296e-011          9.5181         0.25567         0.55535
v  omega                    57.501      2.732e+008     1.2912e+006           76841
v  TempK                    298.58          363.17          338.29          347.47
v  TurbVisc            2.4382e-018       0.0021094     6.6123e-005      0.00023216
v  CourantNb           7.8135e-005          1.5209         0.78776         0.96896
v  FourierNb             0.0037951               1         0.42464         0.19578
v  total_pressure      1.0079e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0037957       7.44e-005      0.00020313

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.62
v  Yplus               0          2.9301         0.62711         0.48218


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62248          2.1247          1.2124          1.1647


 INSTANT    0.952000000E-02   TIME STEP NUMBER             952
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925050E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10289E-01 0.46916E+01
   Friction velocity        uk    :  0.10289E-01 0.46876E+01
   Dimensionless distance   yplus :  0.69759E-02 0.29297E+01
   Friction thermal sca.    tstar :  0.12110E+01 0.25156E+03
   Rough dim-less th. sca.  tplus :  0.49418E-02 0.20754E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26867E+00      11   0.19092E-04   0.63504E+01 0.39391E+02 
c  Velocity[X]                                      0.26163E+01 
c  Velocity[Y]                                      0.16365E+01 
c  Velocity[Z]                                      0.20977E+01 
c  Pressure     0.21492E-04      19   0.37552E-03   0.22328E-01 0.28343E+02 
c  k            0.21128E-01      13   0.95970E-04   0.24907E+00 0.63613E+02 
c  omega        0.27922E+07       1   0.10296E-06   0.19439E+08 0.71679E+00 
c  TempK        0.10041E+05       4   0.47358E-05   0.53058E+01 0.81355E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5756e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.295           19.13        0.002313       -0.013736
v  Velocity[Y]             -15.194          15.104         0.33675         0.49973
v  Velocity[Z]             -25.253           11.73         -1.6374        -0.50574
v  ǁVelocityǁ         0.00042101          25.661          7.6163          6.4995
v  Pressure                -534.03          173.69        -0.99162            4.58
v  k                   9.7292e-011          9.1768         0.25574         0.55549
v  omega                    57.501      2.732e+008     1.2912e+006           76841
v  TempK                    298.58          363.17           338.3          347.48
v  TurbVisc            2.4381e-018       0.0021244     6.6145e-005      0.00023225
v  CourantNb           8.2311e-005          1.5208         0.78776         0.96896
v  FourierNb             0.0037949               1         0.42467         0.19584
v  total_pressure      1.0079e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0038907     7.4402e-005      0.00020315

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.53          306.62
v  Yplus               0          2.9297          0.6271         0.48216


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47927          2.1247          1.2124          1.1648


 INSTANT    0.953000000E-02   TIME STEP NUMBER             953
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925128E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10370E-01 0.46917E+01
   Friction velocity        uk    :  0.10370E-01 0.46877E+01
   Dimensionless distance   yplus :  0.70307E-02 0.29293E+01
   Friction thermal sca.    tstar :  0.12110E+01 0.24960E+03
   Rough dim-less th. sca.  tplus :  0.49806E-02 0.20752E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26866E+00      11   0.19186E-04   0.63519E+01 0.39339E+02 
c  Velocity[X]                                      0.26191E+01 
c  Velocity[Y]                                      0.16386E+01 
c  Velocity[Z]                                      0.20942E+01 
c  Pressure     0.21269E-04      18   0.37698E-03   0.22108E-01 0.28813E+02 
c  k            0.21131E-01      13   0.96263E-04   0.25015E+00 0.63647E+02 
c  omega        0.27922E+07       1   0.10049E-06   0.13657E+08 0.61933E+00 
c  TempK        0.10041E+05       4   0.47342E-05   0.53044E+01 0.81229E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5762e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.295           19.13       0.0023926       -0.013719
v  Velocity[Y]             -15.146          15.107         0.33727         0.50065
v  Velocity[Z]             -25.255          11.857         -1.6375        -0.50574
v  ǁVelocityǁ         0.00042074          25.663           7.616          6.4994
v  Pressure                -533.14          173.54         -1.1377          4.4356
v  k                    9.729e-011          8.8984         0.25581         0.55561
v  omega                    57.501      2.732e+008     1.2912e+006           76841
v  TempK                    298.58          363.17           338.3          347.49
v  TurbVisc             2.438e-018       0.0021386     6.6166e-005      0.00023233
v  CourantNb           8.6511e-005          1.5206         0.78777         0.96897
v  FourierNb             0.0037947               1         0.42469         0.19589
v  total_pressure      1.0079e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0042649     7.4403e-005      0.00020316

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.62
v  Yplus               0          2.9293         0.62709         0.48215


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58641          2.1247          1.2125          1.1649


 INSTANT    0.954000000E-02   TIME STEP NUMBER             954
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925122E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10426E-01 0.46919E+01
   Friction velocity        uk    :  0.10426E-01 0.46879E+01
   Dimensionless distance   yplus :  0.70688E-02 0.29289E+01
   Friction thermal sca.    tstar :  0.12106E+01 0.24825E+03
   Rough dim-less th. sca.  tplus :  0.50076E-02 0.20749E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26866E+00      11   0.19261E-04   0.63488E+01 0.39285E+02 
c  Velocity[X]                                      0.26184E+01 
c  Velocity[Y]                                      0.16418E+01 
c  Velocity[Z]                                      0.20886E+01 
c  Pressure     0.20875E-04      19   0.37716E-03   0.21709E-01 0.28082E+02 
c  k            0.21135E-01      13   0.96094E-04   0.25078E+00 0.63638E+02 
c  omega        0.27922E+07       1   0.10077E-06   0.16670E+08 0.67122E+00 
c  TempK        0.10041E+05       4   0.47317E-05   0.52887E+01 0.81052E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5765e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.295          19.129       0.0024768       -0.013704
v  Velocity[Y]             -15.149           15.11         0.33779         0.50158
v  Velocity[Z]             -25.258          11.723         -1.6375        -0.50575
v  ǁVelocityǁ         0.00042075          25.666          7.6157          6.4993
v  Pressure                -532.21           173.4         -1.2787          4.2962
v  k                   9.7287e-011          8.5955         0.25588         0.55573
v  omega                    57.501      2.732e+008     1.2912e+006           76841
v  TempK                    298.58          363.17           338.3          347.49
v  TurbVisc            2.4379e-018       0.0021521     6.6186e-005      0.00023241
v  CourantNb           9.0307e-005          1.5206         0.78777         0.96898
v  FourierNb             0.0037945               1         0.42471         0.19594
v  total_pressure      1.0079e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0043353     7.4403e-005      0.00020316

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.62
v  Yplus               0          2.9289         0.62708         0.48213


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54402          2.1248          1.2125          1.1649


 INSTANT    0.955000000E-02   TIME STEP NUMBER             955
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925179E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10424E-01 0.46920E+01
   Friction velocity        uk    :  0.10424E-01 0.46880E+01
   Dimensionless distance   yplus :  0.62621E-02 0.29285E+01
   Friction thermal sca.    tstar :  0.12105E+01 0.24830E+03
   Rough dim-less th. sca.  tplus :  0.44361E-02 0.20746E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26865E+00      11   0.19338E-04   0.63467E+01 0.39248E+02 
c  Velocity[X]                                      0.26178E+01 
c  Velocity[Y]                                      0.16450E+01 
c  Velocity[Z]                                      0.20838E+01 
c  Pressure     0.20705E-04      19   0.37393E-03   0.21542E-01 0.26045E+02 
c  k            0.21138E-01      13   0.96026E-04   0.25105E+00 0.63619E+02 
c  omega        0.27922E+07       1   0.98537E-07   0.99793E+07 0.54958E+00 
c  TempK        0.10041E+05       4   0.47299E-05   0.52788E+01 0.80898E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5762e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.295          19.129       0.0025639       -0.013688
v  Velocity[Y]             -15.217          15.113         0.33831          0.5025
v  Velocity[Z]             -25.261          11.719         -1.6376        -0.50575
v  ǁVelocityǁ         0.00042042          25.668          7.6154          6.4992
v  Pressure                -531.18          173.27          -1.407          4.1689
v  k                   9.7284e-011          8.4761         0.25594         0.55583
v  omega                    57.501      2.732e+008     1.2912e+006           76840
v  TempK                    298.58          363.17          338.31           347.5
v  TurbVisc            2.4379e-018       0.0021648     6.6204e-005      0.00023248
v  CourantNb           9.3188e-005          1.5206         0.78777         0.96899
v  FourierNb             0.0037943               1         0.42474         0.19598
v  total_pressure      1.0079e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0036788     7.4402e-005      0.00020316

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.62
v  Yplus               0          2.9285         0.62706         0.48211


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40227           2.125          1.2125           1.165


 INSTANT    0.956000000E-02   TIME STEP NUMBER             956
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925149E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10487E-01 0.46921E+01
   Friction velocity        uk    :  0.10486E-01 0.46881E+01
   Dimensionless distance   yplus :  0.71100E-02 0.29281E+01
   Friction thermal sca.    tstar :  0.12106E+01 0.24682E+03
   Rough dim-less th. sca.  tplus :  0.50368E-02 0.20743E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26864E+00      11   0.19375E-04   0.63517E+01 0.39250E+02 
c  Velocity[X]                                      0.26179E+01 
c  Velocity[Y]                                      0.16520E+01 
c  Velocity[Z]                                      0.20818E+01 
c  Pressure     0.20558E-04      19   0.37406E-03   0.21399E-01 0.24041E+02 
c  k            0.21141E-01      13   0.96043E-04   0.25156E+00 0.63639E+02 
c  omega        0.27922E+07       1   0.10038E-06   0.14581E+08 0.63471E+00 
c  TempK        0.10042E+05       4   0.47290E-05   0.52751E+01 0.80777E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5755e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.294          19.128       0.0026547       -0.013669
v  Velocity[Y]             -15.287          15.116         0.33884         0.50341
v  Velocity[Z]             -25.263          11.715         -1.6377        -0.50576
v  ǁVelocityǁ         0.00042042          25.671          7.6151          6.4991
v  Pressure                -530.08          173.16         -1.5207           4.056
v  k                   9.7282e-011          8.3282           0.256         0.55592
v  omega                    57.501      2.732e+008     1.2912e+006           76840
v  TempK                    298.58          363.17          338.31          347.51
v  TurbVisc            2.4378e-018       0.0021767     6.6221e-005      0.00023255
v  CourantNb           9.5812e-005          1.5208         0.78776           0.969
v  FourierNb             0.0037941               1         0.42475         0.19601
v  total_pressure      1.0079e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0031938       7.44e-005      0.00020315

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.62
v  Yplus               0          2.9281         0.62706          0.4821


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43815          2.1253          1.2125           1.165


 INSTANT    0.957000000E-02   TIME STEP NUMBER             957
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925079E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10488E-01 0.46922E+01
   Friction velocity        uk    :  0.10488E-01 0.46882E+01
   Dimensionless distance   yplus :  0.71112E-02 0.29276E+01
   Friction thermal sca.    tstar :  0.12108E+01 0.24678E+03
   Rough dim-less th. sca.  tplus :  0.50376E-02 0.20740E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26864E+00      11   0.19380E-04   0.63573E+01 0.39250E+02 
c  Velocity[X]                                      0.26179E+01 
c  Velocity[Y]                                      0.16594E+01 
c  Velocity[Z]                                      0.20801E+01 
c  Pressure     0.20514E-04      19   0.37248E-03   0.21362E-01 0.22749E+02 
c  k            0.21144E-01      13   0.95878E-04   0.25193E+00 0.63631E+02 
c  omega        0.27922E+07       1   0.99592E-07   0.13698E+08 0.61845E+00 
c  TempK        0.10042E+05       4   0.47287E-05   0.52798E+01 0.80665E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5755e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.294          19.128       0.0027475       -0.013648
v  Velocity[Y]             -15.272           15.12         0.33936         0.50432
v  Velocity[Z]             -25.266          12.698         -1.6378        -0.50577
v  ǁVelocityǁ         0.00042018          25.673          7.6148          6.4991
v  Pressure                -528.92          173.05         -1.6264          3.9514
v  k                   9.7279e-011          8.1325         0.25606           0.556
v  omega                    57.501      2.732e+008     1.2912e+006           76840
v  TempK                    298.58          363.17          338.31          347.51
v  TurbVisc            2.4377e-018       0.0021877     6.6237e-005      0.00023261
v  CourantNb           9.8677e-005          1.5208         0.78776         0.96901
v  FourierNb              0.003794               1         0.42477         0.19604
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0032117     7.4398e-005      0.00020314

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.62
v  Yplus               0          2.9276         0.62704         0.48208


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46227          2.1254          1.2125          1.1651


 INSTANT    0.958000000E-02   TIME STEP NUMBER             958
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925168E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10535E-01 0.46923E+01
   Friction velocity        uk    :  0.10535E-01 0.46883E+01
   Dimensionless distance   yplus :  0.71426E-02 0.29272E+01
   Friction thermal sca.    tstar :  0.12108E+01 0.24569E+03
   Rough dim-less th. sca.  tplus :  0.50599E-02 0.20737E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26863E+00      11   0.19418E-04   0.63769E+01 0.39250E+02 
c  Velocity[X]                                      0.26177E+01 
c  Velocity[Y]                                      0.16626E+01 
c  Velocity[Z]                                      0.20966E+01 
c  Pressure     0.20490E-04      19   0.37064E-03   0.21347E-01 0.22365E+02 
c  k            0.21146E-01      13   0.95826E-04   0.25184E+00 0.63581E+02 
c  omega        0.27922E+07       1   0.99927E-07   0.14604E+08 0.63223E+00 
c  TempK        0.10042E+05       4   0.47282E-05   0.52891E+01 0.80579E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5754e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.293          19.127        0.002846       -0.013623
v  Velocity[Y]             -15.183          15.124          0.3399         0.50523
v  Velocity[Z]             -25.269          11.708         -1.6379        -0.50578
v  ǁVelocityǁ         0.00042003          25.675          7.6146          6.4991
v  Pressure                 -527.7          172.95         -1.7291          3.8495
v  k                   9.7277e-011           8.294         0.25611         0.55606
v  omega                    57.501      2.732e+008     1.2912e+006           76840
v  TempK                    298.58          363.17          338.32          347.52
v  TurbVisc            2.4377e-018       0.0021977     6.6252e-005      0.00023267
v  CourantNb            0.00011465          1.5208         0.78776         0.96902
v  FourierNb             0.0037938               1         0.42479         0.19606
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0032251     7.4394e-005      0.00020313

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.62
v  Yplus               0          2.9272         0.62703         0.48206


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51419          2.1256          1.2126          1.1651


 INSTANT    0.959000000E-02   TIME STEP NUMBER             959
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925136E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10563E-01 0.46924E+01
   Friction velocity        uk    :  0.10563E-01 0.46884E+01
   Dimensionless distance   yplus :  0.71622E-02 0.29268E+01
   Friction thermal sca.    tstar :  0.12102E+01 0.24502E+03
   Rough dim-less th. sca.  tplus :  0.50737E-02 0.20734E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26863E+00      11   0.19464E-04   0.63603E+01 0.39243E+02 
c  Velocity[X]                                      0.26152E+01 
c  Velocity[Y]                                      0.16714E+01 
c  Velocity[Z]                                      0.20737E+01 
c  Pressure     0.19926E-04      18   0.37308E-03   0.20768E-01 0.20946E+02 
c  k            0.21149E-01      13   0.95979E-04   0.25157E+00 0.63549E+02 
c  omega        0.27922E+07       1   0.99779E-07   0.13959E+08 0.61994E+00 
c  TempK        0.10042E+05       4   0.47279E-05   0.52974E+01 0.80520E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5749e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.293          19.127       0.0029471       -0.013593
v  Velocity[Y]             -15.152          15.128         0.34044         0.50613
v  Velocity[Z]             -25.272          11.706          -1.638         -0.5058
v  ǁVelocityǁ         0.00041962          25.678          7.6143          6.4991
v  Pressure                -526.41          172.86         -1.8204          3.7584
v  k                   9.7275e-011           8.624         0.25616         0.55612
v  omega                    57.501      2.732e+008     1.2912e+006           76840
v  TempK                    298.57          363.17          338.32          347.53
v  TurbVisc            2.4376e-018       0.0022066     6.6267e-005      0.00023272
v  CourantNb            0.00013166          1.5209         0.78776         0.96903
v  FourierNb             0.0037936               1          0.4248         0.19607
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0032343     7.4391e-005      0.00020311

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.62
v  Yplus               0          2.9268         0.62702         0.48205


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47358          2.1258          1.2126          1.1651


 INSTANT    0.960000000E-02   TIME STEP NUMBER             960
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925156E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10643E-01 0.46925E+01
   Friction velocity        uk    :  0.10643E-01 0.46885E+01
   Dimensionless distance   yplus :  0.72163E-02 0.29264E+01
   Friction thermal sca.    tstar :  0.12102E+01 0.24319E+03
   Rough dim-less th. sca.  tplus :  0.51121E-02 0.20731E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26862E+00      11   0.19530E-04   0.63561E+01 0.39222E+02 
c  Velocity[X]                                      0.26142E+01 
c  Velocity[Y]                                      0.16765E+01 
c  Velocity[Z]                                      0.20654E+01 
c  Pressure     0.19987E-04      18   0.38075E-03   0.20841E-01 0.21162E+02 
c  k            0.21151E-01      13   0.95232E-04   0.25083E+00 0.63487E+02 
c  omega        0.27922E+07       1   0.99873E-07   0.14385E+08 0.62890E+00 
c  TempK        0.10042E+05       4   0.47256E-05   0.53009E+01 0.80478E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5739e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.292          19.126       0.0030479        -0.01356
v  Velocity[Y]             -15.179          15.133         0.34099         0.50702
v  Velocity[Z]             -25.275          11.703         -1.6381        -0.50581
v  ǁVelocityǁ         0.00041972          25.681          7.6141          6.4991
v  Pressure                -525.07          172.77         -1.9138          3.6659
v  k                   9.7273e-011          8.5275         0.25621         0.55616
v  omega                    57.501      2.732e+008     1.2912e+006           76840
v  TempK                    298.57          363.17          338.33          347.53
v  TurbVisc            2.4376e-018       0.0022144     6.6281e-005      0.00023276
v  CourantNb            0.00012906          1.5212         0.78776         0.96903
v  FourierNb             0.0037934               1         0.42482         0.19607
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0032992     7.4388e-005      0.00020309

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.62
v  Yplus               0          2.9264         0.62701         0.48203


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.31981          2.1262          1.2126          1.1651


 INSTANT    0.961000000E-02   TIME STEP NUMBER             961
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925098E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10629E-01 0.46926E+01
   Friction velocity        uk    :  0.10629E-01 0.46886E+01
   Dimensionless distance   yplus :  0.72068E-02 0.29259E+01
   Friction thermal sca.    tstar :  0.12100E+01 0.24351E+03
   Rough dim-less th. sca.  tplus :  0.51053E-02 0.20728E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26862E+00      11   0.19535E-04   0.63445E+01 0.39185E+02 
c  Velocity[X]                                      0.26116E+01 
c  Velocity[Y]                                      0.16794E+01 
c  Velocity[Z]                                      0.20536E+01 
c  Pressure     0.19687E-04      18   0.38329E-03   0.20538E-01 0.20064E+02 
c  k            0.21153E-01      13   0.95056E-04   0.24990E+00 0.63433E+02 
c  omega        0.27922E+07       1   0.98355E-07   0.10455E+08 0.55647E+00 
c  TempK        0.10043E+05       4   0.47218E-05   0.52962E+01 0.80450E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5723e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.291          19.126       0.0031516       -0.013523
v  Velocity[Y]             -15.242          15.137         0.34154         0.50791
v  Velocity[Z]             -25.278            11.7         -1.6383        -0.50581
v  ǁVelocityǁ         0.00041956          25.683          7.6139          6.4992
v  Pressure                -523.66          172.68         -1.9993          3.5809
v  k                   9.7271e-011          8.3959         0.25626         0.55619
v  omega                    57.501      2.732e+008     1.2912e+006           76840
v  TempK                    298.57          363.17          338.33          347.54
v  TurbVisc            2.4375e-018       0.0022208     6.6294e-005       0.0002328
v  CourantNb            0.00013282          1.5215         0.78776         0.96904
v  FourierNb             0.0037932               1         0.42483         0.19607
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0033962     7.4385e-005      0.00020307

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.62
v  Yplus               0          2.9259           0.627         0.48201


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40044          2.1268          1.2126          1.1651


 INSTANT    0.962000000E-02   TIME STEP NUMBER             962
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925235E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10659E-01 0.46926E+01
   Friction velocity        uk    :  0.10659E-01 0.46886E+01
   Dimensionless distance   yplus :  0.72268E-02 0.29255E+01
   Friction thermal sca.    tstar :  0.12100E+01 0.24284E+03
   Rough dim-less th. sca.  tplus :  0.51195E-02 0.20725E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26861E+00      11   0.19532E-04   0.63440E+01 0.39199E+02 
c  Velocity[X]                                      0.26099E+01 
c  Velocity[Y]                                      0.16838E+01 
c  Velocity[Z]                                      0.20502E+01 
c  Pressure     0.19401E-04      18   0.37586E-03   0.20248E-01 0.18479E+02 
c  k            0.21155E-01      13   0.94674E-04   0.24893E+00 0.63389E+02 
c  omega        0.27922E+07       1   0.99704E-07   0.13262E+08 0.60907E+00 
c  TempK        0.10043E+05       4   0.47187E-05   0.52922E+01 0.80463E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5703e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.29          19.126       0.0032596       -0.013484
v  Velocity[Y]              -15.34          15.142         0.34209         0.50879
v  Velocity[Z]             -25.281          11.697         -1.6384        -0.50582
v  ǁVelocityǁ         0.00041956          25.686          7.6136          6.4993
v  Pressure                -522.19          172.61         -2.0731          3.5072
v  k                    9.727e-011          8.1921          0.2563         0.55621
v  omega                    57.501      2.732e+008     1.2912e+006           76840
v  TempK                    298.56          363.17          338.33          347.55
v  TurbVisc            2.4375e-018       0.0022259     6.6306e-005      0.00023284
v  CourantNb            0.00014888           1.522         0.78776         0.96905
v  FourierNb              0.003793               1         0.42484         0.19607
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034461      7.438e-005      0.00020305

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.62
v  Yplus               0          2.9255           0.627           0.482


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45318          2.1273          1.2126          1.1651


 INSTANT    0.963000000E-02   TIME STEP NUMBER             963
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925248E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10661E-01 0.46927E+01
   Friction velocity        uk    :  0.10661E-01 0.46887E+01
   Dimensionless distance   yplus :  0.72283E-02 0.29251E+01
   Friction thermal sca.    tstar :  0.12102E+01 0.24278E+03
   Rough dim-less th. sca.  tplus :  0.51206E-02 0.20721E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26861E+00      11   0.19539E-04   0.63443E+01 0.39227E+02 
c  Velocity[X]                                      0.26090E+01 
c  Velocity[Y]                                      0.16919E+01 
c  Velocity[Z]                                      0.20435E+01 
c  Pressure     0.19280E-04      18   0.37867E-03   0.20128E-01 0.18023E+02 
c  k            0.21157E-01      13   0.94131E-04   0.24778E+00 0.63315E+02 
c  omega        0.27922E+07       1   0.10029E-06   0.15536E+08 0.65142E+00 
c  TempK        0.10043E+05       4   0.47189E-05   0.52932E+01 0.80470E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5689e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.289          19.125        0.003369        -0.01344
v  Velocity[Y]             -15.311          15.147         0.34265         0.50966
v  Velocity[Z]             -25.283          11.694         -1.6385        -0.50582
v  ǁVelocityǁ         0.00041943          25.689          7.6134          6.4994
v  Pressure                -520.65          172.54         -2.1428           3.438
v  k                   9.7268e-011           7.964         0.25634         0.55621
v  omega                      57.5      2.732e+008     1.2912e+006           76839
v  TempK                    298.56          363.17          338.34          347.55
v  TurbVisc            2.4374e-018       0.0022294     6.6317e-005      0.00023287
v  CourantNb             0.0001622          1.5223         0.78776         0.96906
v  FourierNb             0.0037928               1         0.42485         0.19606
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034696     7.4377e-005      0.00020303

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.62
v  Yplus               0          2.9251         0.62699         0.48199


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48205          2.1278          1.2126          1.1651


 INSTANT    0.964000000E-02   TIME STEP NUMBER             964
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925258E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84663E-02 0.46928E+01
   Friction velocity        uk    :  0.84663E-02 0.46887E+01
   Dimensionless distance   yplus :  0.57403E-02 0.29246E+01
   Friction thermal sca.    tstar :  0.12103E+01 0.30338E+03
   Rough dim-less th. sca.  tplus :  0.40664E-02 0.20718E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26860E+00      11   0.19491E-04   0.63337E+01 0.39194E+02 
c  Velocity[X]                                      0.26060E+01 
c  Velocity[Y]                                      0.16913E+01 
c  Velocity[Z]                                      0.20364E+01 
c  Pressure     0.19046E-04      18   0.37373E-03   0.19889E-01 0.17630E+02 
c  k            0.21158E-01      13   0.93711E-04   0.24666E+00 0.63243E+02 
c  omega        0.27922E+07       1   0.99483E-07   0.13890E+08 0.62277E+00 
c  TempK        0.10044E+05       4   0.47199E-05   0.52989E+01 0.80506E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5674e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.288          19.125       0.0034837       -0.013392
v  Velocity[Y]             -15.279          15.152         0.34321         0.51054
v  Velocity[Z]             -25.287           11.69         -1.6387        -0.50583
v  ǁVelocityǁ         0.00041939          25.691          7.6132          6.4995
v  Pressure                -519.04          172.47          -2.209          3.3725
v  k                   9.7267e-011          8.1441         0.25638         0.55621
v  omega                      57.5      2.732e+008     1.2912e+006           76839
v  TempK                    298.55          363.17          338.34          347.56
v  TurbVisc            2.4374e-018       0.0022311     6.6326e-005       0.0002329
v  CourantNb             0.0001757          1.5227         0.78776         0.96907
v  FourierNb             0.0037926               1         0.42486         0.19604
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034802     7.4373e-005      0.00020301

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.62
v  Yplus               0          2.9246         0.62699         0.48197


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44301          2.1283          1.2126          1.1651


 INSTANT    0.965000000E-02   TIME STEP NUMBER             965
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925338E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70864E-02 0.46928E+01
   Friction velocity        uk    :  0.70864E-02 0.46888E+01
   Dimensionless distance   yplus :  0.48047E-02 0.29242E+01
   Friction thermal sca.    tstar :  0.12096E+01 0.36246E+03
   Rough dim-less th. sca.  tplus :  0.34037E-02 0.20715E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26860E+00      11   0.19376E-04   0.63329E+01 0.39221E+02 
c  Velocity[X]                                      0.26053E+01 
c  Velocity[Y]                                      0.16975E+01 
c  Velocity[Z]                                      0.20301E+01 
c  Pressure     0.18979E-04      18   0.37817E-03   0.19825E-01 0.17405E+02 
c  k            0.21160E-01      13   0.93564E-04   0.24576E+00 0.63201E+02 
c  omega        0.27922E+07       1   0.10046E-06   0.15497E+08 0.64776E+00 
c  TempK        0.10044E+05       4   0.47177E-05   0.53071E+01 0.80560E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5656e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.287          19.125       0.0036021       -0.013337
v  Velocity[Y]              -15.26          15.158         0.34378         0.51141
v  Velocity[Z]              -25.29          11.686         -1.6388        -0.50585
v  ǁVelocityǁ         0.00041899          25.694          7.6131          6.4996
v  Pressure                -517.36          172.41         -2.2717          3.3098
v  k                   9.7266e-011          8.5112         0.25641         0.55619
v  omega                      57.5      2.732e+008     1.2912e+006           76839
v  TempK                    298.55          363.17          338.34          347.57
v  TurbVisc            2.4374e-018       0.0022311     6.6334e-005      0.00023292
v  CourantNb            0.00018052          1.5231         0.78776         0.96909
v  FourierNb             0.0037924               1         0.42487         0.19602
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034821     7.4368e-005      0.00020299

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.62
v  Yplus               0          2.9242         0.62698         0.48196


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39789          2.1288          1.2126          1.1651


 INSTANT    0.966000000E-02   TIME STEP NUMBER             966
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925273E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87309E-02 0.46928E+01
   Friction velocity        uk    :  0.87309E-02 0.46888E+01
   Dimensionless distance   yplus :  0.59197E-02 0.29238E+01
   Friction thermal sca.    tstar :  0.12096E+01 0.29419E+03
   Rough dim-less th. sca.  tplus :  0.41936E-02 0.20712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26860E+00      11   0.19361E-04   0.63312E+01 0.39238E+02 
c  Velocity[X]                                      0.26059E+01 
c  Velocity[Y]                                      0.17011E+01 
c  Velocity[Z]                                      0.20242E+01 
c  Pressure     0.19045E-04      18   0.37030E-03   0.19898E-01 0.17610E+02 
c  k            0.21161E-01      13   0.93372E-04   0.24493E+00 0.63166E+02 
c  omega        0.27922E+07       1   0.99502E-07   0.13684E+08 0.61844E+00 
c  TempK        0.10044E+05       4   0.47179E-05   0.53223E+01 0.80617E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5634e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.286          19.125       0.0037225       -0.013281
v  Velocity[Y]             -15.294          15.164         0.34436         0.51227
v  Velocity[Z]             -25.293          11.682         -1.6389        -0.50587
v  ǁVelocityǁ         0.00041904          25.697          7.6129          6.4998
v  Pressure                -515.59          172.35         -2.3374          3.2446
v  k                   9.7265e-011          8.4242         0.25645         0.55617
v  omega                      57.5      2.732e+008     1.2912e+006           76839
v  TempK                    298.55          363.17          338.35          347.57
v  TurbVisc            2.4373e-018       0.0022232      6.634e-005      0.00023293
v  CourantNb            0.00018083          1.5236         0.78777          0.9691
v  FourierNb             0.0037922               1         0.42487         0.19599
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0032974     7.4362e-005      0.00020296

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.62
v  Yplus               0          2.9238         0.62697         0.48195


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5213          2.1295          1.2126          1.1651


 INSTANT    0.967000000E-02   TIME STEP NUMBER             967
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925144E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10769E-01 0.46929E+01
   Friction velocity        uk    :  0.10769E-01 0.46888E+01
   Dimensionless distance   yplus :  0.73015E-02 0.29234E+01
   Friction thermal sca.    tstar :  0.12096E+01 0.24036E+03
   Rough dim-less th. sca.  tplus :  0.51724E-02 0.20709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26860E+00      11   0.19268E-04   0.63207E+01 0.39226E+02 
c  Velocity[X]                                      0.26038E+01 
c  Velocity[Y]                                      0.17021E+01 
c  Velocity[Z]                                      0.20148E+01 
c  Pressure     0.19196E-04      18   0.36363E-03   0.20061E-01 0.17296E+02 
c  k            0.21162E-01      13   0.93128E-04   0.24405E+00 0.63157E+02 
c  omega        0.27922E+07       1   0.10224E-06   0.21921E+08 0.75008E+00 
c  TempK        0.10045E+05       4   0.47173E-05   0.53384E+01 0.80670E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5605e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.285          19.124       0.0038465        -0.01322
v  Velocity[Y]             -15.375           15.17         0.34494         0.51313
v  Velocity[Z]             -25.296          11.678         -1.6391        -0.50589
v  ǁVelocityǁ         0.00041905            25.7          7.6127             6.5
v  Pressure                -513.72          172.29         -2.4006          3.1812
v  k                   9.7264e-011           8.307         0.25648         0.55614
v  omega                      57.5      2.732e+008     1.2912e+006           76839
v  TempK                    298.55          363.17          338.35          347.58
v  TurbVisc            2.4373e-018       0.0022242     6.6346e-005      0.00023294
v  CourantNb            0.00018189          1.5243         0.78777         0.96912
v  FourierNb              0.003792               1         0.42488         0.19595
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0033439     7.4357e-005      0.00020293

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.63
v  Yplus               0          2.9234         0.62697         0.48195


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58625          2.1303          1.2126          1.1651


 INSTANT    0.968000000E-02   TIME STEP NUMBER             968
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925185E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10770E-01 0.46929E+01
   Friction velocity        uk    :  0.10770E-01 0.46889E+01
   Dimensionless distance   yplus :  0.73023E-02 0.29229E+01
   Friction thermal sca.    tstar :  0.12097E+01 0.24033E+03
   Rough dim-less th. sca.  tplus :  0.51730E-02 0.20706E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26859E+00      11   0.19112E-04   0.63127E+01 0.39234E+02 
c  Velocity[X]                                      0.26021E+01 
c  Velocity[Y]                                      0.17035E+01 
c  Velocity[Z]                                      0.20071E+01 
c  Pressure     0.18903E-04      18   0.36180E-03   0.19759E-01 0.16063E+02 
c  k            0.21163E-01      13   0.92919E-04   0.24312E+00 0.63154E+02 
c  omega        0.27922E+07       1   0.99657E-07   0.13265E+08 0.60845E+00 
c  TempK        0.10045E+05       4   0.47168E-05   0.53472E+01 0.80720E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5577e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.284          19.124        0.003973       -0.013158
v  Velocity[Y]              -15.48          15.175         0.34551         0.51399
v  Velocity[Z]             -25.299          11.676         -1.6393        -0.50591
v  ǁVelocityǁ         0.00041906          25.703          7.6126          6.5001
v  Pressure                -511.74          172.24         -2.4533          3.1285
v  k                   9.7264e-011          8.1455         0.25651         0.55611
v  omega                      57.5      2.732e+008     1.2912e+006           76839
v  TempK                    298.54          363.17          338.35          347.59
v  TurbVisc            2.4373e-018       0.0022193     6.6351e-005      0.00023295
v  CourantNb            0.00018316          1.5249         0.78777         0.96913
v  FourierNb             0.0037918               1         0.42488         0.19592
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006        0.003368     7.4352e-005       0.0002029

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.63
v  Yplus               0          2.9229         0.62697         0.48194


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40795          2.1311          1.2127          1.1651


 INSTANT    0.969000000E-02   TIME STEP NUMBER             969
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925170E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10769E-01 0.46929E+01
   Friction velocity        uk    :  0.10769E-01 0.46889E+01
   Dimensionless distance   yplus :  0.73013E-02 0.29225E+01
   Friction thermal sca.    tstar :  0.12100E+01 0.24036E+03
   Rough dim-less th. sca.  tplus :  0.51723E-02 0.20703E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26859E+00      11   0.18989E-04   0.62981E+01 0.39238E+02 
c  Velocity[X]                                      0.25989E+01 
c  Velocity[Y]                                      0.17046E+01 
c  Velocity[Z]                                      0.19947E+01 
c  Pressure     0.18636E-04      18   0.35612E-03   0.19484E-01 0.15749E+02 
c  k            0.21164E-01      13   0.92878E-04   0.24216E+00 0.63143E+02 
c  omega        0.27922E+07       1   0.99196E-07   0.11754E+08 0.58740E+00 
c  TempK        0.10045E+05       4   0.47141E-05   0.53504E+01 0.80760E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5553e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.282          19.124       0.0041014       -0.013095
v  Velocity[Y]             -15.468          15.181         0.34609         0.51484
v  Velocity[Z]             -25.302          11.674         -1.6394        -0.50593
v  ǁVelocityǁ         0.00041897          25.705          7.6125          6.5003
v  Pressure                -509.69          172.18         -2.5041          3.0776
v  k                   9.7263e-011          7.9855         0.25654         0.55607
v  omega                      57.5      2.732e+008     1.2912e+006           76839
v  TempK                    298.54          363.17          338.36          347.59
v  TurbVisc            2.4373e-018       0.0022102     6.6355e-005      0.00023295
v  CourantNb            0.00018336          1.5255         0.78778         0.96915
v  FourierNb             0.0037917               1         0.42488         0.19588
v  total_pressure      1.0082e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0033805     7.4346e-005      0.00020288

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.63
v  Yplus               0          2.9225         0.62697         0.48194


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.34488          2.1317          1.2127           1.165


 INSTANT    0.970000000E-02   TIME STEP NUMBER             970
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925275E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10789E-01 0.46929E+01
   Friction velocity        uk    :  0.10789E-01 0.46889E+01
   Dimensionless distance   yplus :  0.73151E-02 0.29221E+01
   Friction thermal sca.    tstar :  0.12100E+01 0.23991E+03
   Rough dim-less th. sca.  tplus :  0.51821E-02 0.20700E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26859E+00      11   0.18906E-04   0.62804E+01 0.39214E+02 
c  Velocity[X]                                      0.25923E+01 
c  Velocity[Y]                                      0.17029E+01 
c  Velocity[Z]                                      0.19852E+01 
c  Pressure     0.18569E-04      18   0.34610E-03   0.19417E-01 0.15562E+02 
c  k            0.21164E-01      13   0.92650E-04   0.24136E+00 0.63142E+02 
c  omega        0.27922E+07       1   0.99906E-07   0.14568E+08 0.63796E+00 
c  TempK        0.10046E+05       4   0.47110E-05   0.53563E+01 0.80783E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5529e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.281          19.124       0.0042306       -0.013031
v  Velocity[Y]             -15.394          15.188         0.34667         0.51568
v  Velocity[Z]             -25.305          11.671         -1.6396        -0.50596
v  ǁVelocityǁ         0.00041909          25.708          7.6123          6.5005
v  Pressure                -507.59          172.14         -2.5523          3.0298
v  k                   9.7263e-011          8.3099         0.25657         0.55602
v  omega                      57.5      2.732e+008     1.2912e+006           76839
v  TempK                    298.54          363.17          338.36           347.6
v  TurbVisc            2.4373e-018       0.0022044     6.6358e-005      0.00023295
v  CourantNb            0.00017887           1.526         0.78778         0.96917
v  FourierNb             0.0037915               1         0.42488         0.19584
v  total_pressure      1.0082e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0033986      7.434e-005      0.00020285

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.63
v  Yplus               0          2.9221         0.62697         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58727          2.1324          1.2127           1.165


 INSTANT    0.971000000E-02   TIME STEP NUMBER             971
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925197E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10769E-01 0.46929E+01
   Friction velocity        uk    :  0.10769E-01 0.46889E+01
   Dimensionless distance   yplus :  0.73017E-02 0.29217E+01
   Friction thermal sca.    tstar :  0.12094E+01 0.24035E+03
   Rough dim-less th. sca.  tplus :  0.51726E-02 0.20697E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26858E+00      11   0.18850E-04   0.62587E+01 0.39184E+02 
c  Velocity[X]                                      0.25861E+01 
c  Velocity[Y]                                      0.17004E+01 
c  Velocity[Z]                                      0.19722E+01 
c  Pressure     0.18357E-04      18   0.33701E-03   0.19198E-01 0.14984E+02 
c  k            0.21164E-01      13   0.92498E-04   0.24080E+00 0.63166E+02 
c  omega        0.27922E+07       1   0.98798E-07   0.11598E+08 0.58544E+00 
c  TempK        0.10046E+05       4   0.47088E-05   0.53651E+01 0.80835E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5502e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.28          19.125       0.0043615       -0.012963
v  Velocity[Y]             -15.381          15.194         0.34725         0.51652
v  Velocity[Z]             -25.309          11.669         -1.6397        -0.50599
v  ǁVelocityǁ          0.0002253          25.711          7.6122          6.5007
v  Pressure                -505.45           172.1         -2.5946          2.9872
v  k                   9.7263e-011          8.8313         0.25661         0.55598
v  omega                      57.5      2.732e+008     1.2912e+006           76838
v  TempK                    298.54          363.17          338.36          347.61
v  TurbVisc            2.4373e-018       0.0022097     6.6361e-005      0.00023294
v  CourantNb            0.00019099          1.5267         0.78779         0.96919
v  FourierNb             0.0037913               1         0.42488          0.1958
v  total_pressure      1.0082e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034224     7.4335e-005      0.00020282

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.54          306.63
v  Yplus               0          2.9217         0.62697         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47413          2.1331          1.2127           1.165


 INSTANT    0.972000000E-02   TIME STEP NUMBER             972
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925172E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10797E-01 0.46929E+01
   Friction velocity        uk    :  0.10797E-01 0.46889E+01
   Dimensionless distance   yplus :  0.73206E-02 0.29213E+01
   Friction thermal sca.    tstar :  0.12094E+01 0.23973E+03
   Rough dim-less th. sca.  tplus :  0.51860E-02 0.20694E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26858E+00      11   0.18790E-04   0.62428E+01 0.39187E+02 
c  Velocity[X]                                      0.25793E+01 
c  Velocity[Y]                                      0.17019E+01 
c  Velocity[Z]                                      0.19615E+01 
c  Pressure     0.18298E-04      18   0.33356E-03   0.19137E-01 0.14457E+02 
c  k            0.21164E-01      13   0.92376E-04   0.24013E+00 0.63149E+02 
c  omega        0.27922E+07       1   0.10065E-06   0.15505E+08 0.65523E+00 
c  TempK        0.10046E+05       4   0.47063E-05   0.53580E+01 0.80843E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5471e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.278          19.125       0.0044951       -0.012891
v  Velocity[Y]             -15.426          15.201         0.34784         0.51736
v  Velocity[Z]             -25.312          11.667         -1.6399        -0.50602
v  ǁVelocityǁ         0.00041881          25.714          7.6121          6.5009
v  Pressure                -505.24          172.07         -2.6273          2.9541
v  k                   9.7263e-011          8.7806         0.25664         0.55593
v  omega                      57.5      2.732e+008     1.2912e+006           76838
v  TempK                    298.54          363.17          338.37          347.61
v  TurbVisc            2.4373e-018       0.0022177     6.6363e-005      0.00023294
v  CourantNb            0.00020607          1.5274          0.7878         0.96921
v  FourierNb             0.0037911               1         0.42488         0.19575
v  total_pressure      1.0082e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034509     7.4329e-005      0.00020279

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.55          306.63
v  Yplus               0          2.9213         0.62698         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45532           2.134          1.2127           1.165


 INSTANT    0.973000000E-02   TIME STEP NUMBER             973
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925186E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10827E-01 0.46929E+01
   Friction velocity        uk    :  0.10827E-01 0.46889E+01
   Dimensionless distance   yplus :  0.73411E-02 0.29208E+01
   Friction thermal sca.    tstar :  0.12094E+01 0.23906E+03
   Rough dim-less th. sca.  tplus :  0.52005E-02 0.20691E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26858E+00      11   0.18710E-04   0.62219E+01 0.39173E+02 
c  Velocity[X]                                      0.25734E+01 
c  Velocity[Y]                                      0.17004E+01 
c  Velocity[Z]                                      0.19481E+01 
c  Pressure     0.18045E-04      18   0.33093E-03   0.18874E-01 0.14454E+02 
c  k            0.21164E-01      13   0.92399E-04   0.23957E+00 0.63163E+02 
c  omega        0.27922E+07       1   0.10066E-06   0.16306E+08 0.66984E+00 
c  TempK        0.10047E+05       4   0.47039E-05   0.53515E+01 0.80845E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5434e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.277          19.125       0.0046314       -0.012814
v  Velocity[Y]             -15.515          15.208         0.34843          0.5182
v  Velocity[Z]             -25.315          12.507         -1.6401        -0.50604
v  ǁVelocityǁ         0.00041872          25.717          7.6121          6.5011
v  Pressure                -505.75          172.03         -2.6637          2.9174
v  k                   9.7263e-011           8.643         0.25667         0.55588
v  omega                      57.5      2.732e+008     1.2912e+006           76838
v  TempK                    298.53          363.17          338.37          347.62
v  TurbVisc            2.4373e-018       0.0022219     6.6365e-005      0.00023293
v  CourantNb            0.00022198          1.5283         0.78781         0.96922
v  FourierNb              0.003791               1         0.42488         0.19571
v  total_pressure      1.0082e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034831     7.4323e-005      0.00020276

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.55          306.63
v  Yplus               0          2.9208         0.62698         0.48192


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46035           2.135          1.2127          1.1649


 INSTANT    0.974000000E-02   TIME STEP NUMBER             974
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925202E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10847E-01 0.46929E+01
   Friction velocity        uk    :  0.10847E-01 0.46889E+01
   Dimensionless distance   yplus :  0.73543E-02 0.29204E+01
   Friction thermal sca.    tstar :  0.12095E+01 0.23864E+03
   Rough dim-less th. sca.  tplus :  0.52098E-02 0.20688E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26858E+00      11   0.18664E-04   0.61985E+01 0.39138E+02 
c  Velocity[X]                                      0.25637E+01 
c  Velocity[Y]                                      0.16978E+01 
c  Velocity[Z]                                      0.19369E+01 
c  Pressure     0.18173E-04      17   0.33319E-03   0.19008E-01 0.14255E+02 
c  k            0.21164E-01      13   0.92552E-04   0.23905E+00 0.63184E+02 
c  omega        0.27922E+07       1   0.10322E-06   0.24339E+08 0.79150E+00 
c  TempK        0.10047E+05       4   0.47020E-05   0.53516E+01 0.80869E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5395e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.275          19.126       0.0047697       -0.012735
v  Velocity[Y]             -15.628          15.214         0.34902         0.51904
v  Velocity[Z]             -25.319          13.371         -1.6402        -0.50607
v  ǁVelocityǁ         0.00041894           25.72           7.612          6.5013
v  Pressure                -505.59             172         -2.6986           2.882
v  k                   9.7263e-011          8.3698          0.2567         0.55583
v  omega                      57.5      2.732e+008     1.2912e+006           76838
v  TempK                    298.53          363.17          338.37          347.63
v  TurbVisc            2.4373e-018       0.0022258     6.6367e-005      0.00023292
v  CourantNb            0.00020066          1.5292         0.78781         0.96924
v  FourierNb             0.0037908               1         0.42488         0.19566
v  total_pressure      1.0082e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034376     7.4317e-005      0.00020273

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.55          306.63
v  Yplus               0          2.9204         0.62699         0.48192


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6099           2.136          1.2127          1.1649


 INSTANT    0.975000000E-02   TIME STEP NUMBER             975
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925260E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10807E-01 0.46929E+01
   Friction velocity        uk    :  0.10807E-01 0.46889E+01
   Dimensionless distance   yplus :  0.73272E-02 0.29200E+01
   Friction thermal sca.    tstar :  0.12099E+01 0.23952E+03
   Rough dim-less th. sca.  tplus :  0.51906E-02 0.20686E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26857E+00      11   0.18611E-04   0.61757E+01 0.39112E+02 
c  Velocity[X]                                      0.25568E+01 
c  Velocity[Y]                                      0.16962E+01 
c  Velocity[Z]                                      0.19226E+01 
c  Pressure     0.18179E-04      17   0.33282E-03   0.19015E-01 0.14129E+02 
c  k            0.21163E-01      13   0.92601E-04   0.23847E+00 0.63188E+02 
c  omega        0.27922E+07       1   0.10024E-06   0.15730E+08 0.66384E+00 
c  TempK        0.10047E+05       4   0.47002E-05   0.53551E+01 0.80905E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5362e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.274          19.127       0.0049078       -0.012653
v  Velocity[Y]             -15.614          15.221          0.3496         0.51987
v  Velocity[Z]             -25.322          13.208         -1.6404        -0.50609
v  ǁVelocityǁ         0.00041883          25.722          7.6119          6.5015
v  Pressure                -506.15          171.97         -2.7311          2.8493
v  k                   9.7263e-011          8.0806         0.25673         0.55578
v  omega                    57.499      2.732e+008     1.2912e+006           76838
v  TempK                    298.53          363.17          338.38          347.63
v  TurbVisc            2.4373e-018       0.0022281     6.6369e-005      0.00023291
v  CourantNb            0.00023607          1.5299         0.78781         0.96925
v  FourierNb             0.0037906               1         0.42488         0.19562
v  total_pressure      1.0082e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034836     7.4312e-005       0.0002027

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.55          306.63
v  Yplus               0            2.92         0.62699         0.48192


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55853          2.1369          1.2127          1.1649


 INSTANT    0.976000000E-02   TIME STEP NUMBER             976
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925158E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10830E-01 0.46928E+01
   Friction velocity        uk    :  0.10829E-01 0.46888E+01
   Dimensionless distance   yplus :  0.73426E-02 0.29196E+01
   Friction thermal sca.    tstar :  0.12099E+01 0.23902E+03
   Rough dim-less th. sca.  tplus :  0.52015E-02 0.20683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26857E+00      11   0.18414E-04   0.61498E+01 0.39043E+02 
c  Velocity[X]                                      0.25496E+01 
c  Velocity[Y]                                      0.16885E+01 
c  Velocity[Z]                                      0.19118E+01 
c  Pressure     0.18347E-04      18   0.34359E-03   0.19191E-01 0.13588E+02 
c  k            0.21162E-01      13   0.92697E-04   0.23779E+00 0.63181E+02 
c  omega        0.27922E+07       1   0.99016E-07   0.12431E+08 0.60727E+00 
c  TempK        0.10048E+05       4   0.46987E-05   0.53635E+01 0.80975E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.533e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.272          19.128       0.0050475        -0.01257
v  Velocity[Y]             -15.539          15.228         0.35019          0.5207
v  Velocity[Z]             -25.325          11.659         -1.6406        -0.50611
v  ǁVelocityǁ         0.00041897          25.725          7.6118          6.5017
v  Pressure                -507.03          171.94         -2.7546          2.8261
v  k                   9.7263e-011          8.3217         0.25676         0.55572
v  omega                    57.499      2.732e+008     1.2912e+006           76838
v  TempK                    298.53          363.17          338.38          347.64
v  TurbVisc            2.4373e-018       0.0022268     6.6372e-005       0.0002329
v  CourantNb            0.00022625          1.5307         0.78782         0.96926
v  FourierNb             0.0037905               1         0.42488         0.19558
v  total_pressure      1.0082e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0035337     7.4307e-005      0.00020268

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.55          306.63
v  Yplus               0          2.9196           0.627         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54573          2.1377          1.2127          1.1648


 INSTANT    0.977000000E-02   TIME STEP NUMBER             977
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925253E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10808E-01 0.46928E+01
   Friction velocity        uk    :  0.10808E-01 0.46888E+01
   Dimensionless distance   yplus :  0.73283E-02 0.29192E+01
   Friction thermal sca.    tstar :  0.12093E+01 0.23948E+03
   Rough dim-less th. sca.  tplus :  0.51914E-02 0.20680E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         54 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26857E+00      11   0.18252E-04   0.61235E+01 0.38993E+02 
c  Velocity[X]                                      0.25425E+01 
c  Velocity[Y]                                      0.16825E+01 
c  Velocity[Z]                                      0.18985E+01 
c  Pressure     0.18679E-04      18   0.34982E-03   0.19540E-01 0.13759E+02 
c  k            0.21161E-01      13   0.92521E-04   0.23717E+00 0.63182E+02 
c  omega        0.27922E+07       1   0.97851E-07   0.91341E+07 0.54565E+00 
c  TempK        0.10048E+05       4   0.46967E-05   0.53730E+01 0.81070E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5295e-007                             5


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.27          19.129       0.0051879       -0.012484
v  Velocity[Y]             -15.531          15.235         0.35078         0.52153
v  Velocity[Z]             -25.328          13.385         -1.6407        -0.50613
v  ǁVelocityǁ         0.00041891          25.728          7.6118          6.5019
v  Pressure                -507.86          171.91         -2.7829          2.7977
v  k                   9.7264e-011          8.6914          0.2568         0.55567
v  omega                    57.499      2.732e+008     1.2912e+006           76838
v  TempK                    298.53          363.17          338.38          347.65
v  TurbVisc            2.4373e-018       0.0021995     6.6374e-005      0.00023288
v  CourantNb             0.0001943          1.5315         0.78782         0.96928
v  FourierNb             0.0037903               1         0.42488         0.19554
v  total_pressure      1.0082e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0035866     7.4302e-005      0.00020265

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.55          306.63
v  Yplus               0          2.9192         0.62701         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44953          2.1386          1.2127          1.1648


 INSTANT    0.978000000E-02   TIME STEP NUMBER             978
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925182E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10821E-01 0.46928E+01
   Friction velocity        uk    :  0.10821E-01 0.46888E+01
   Dimensionless distance   yplus :  0.73370E-02 0.29188E+01
   Friction thermal sca.    tstar :  0.12094E+01 0.23920E+03
   Rough dim-less th. sca.  tplus :  0.51975E-02 0.20677E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26857E+00      11   0.18075E-04   0.61095E+01 0.38969E+02 
c  Velocity[X]                                      0.25371E+01 
c  Velocity[Y]                                      0.16772E+01 
c  Velocity[Z]                                      0.18953E+01 
c  Pressure     0.19254E-04      17   0.35040E-03   0.20143E-01 0.13162E+02 
c  k            0.21161E-01      13   0.92199E-04   0.23644E+00 0.63157E+02 
c  omega        0.27922E+07       1   0.98730E-07   0.11411E+08 0.59144E+00 
c  TempK        0.10048E+05       4   0.46945E-05   0.53803E+01 0.81155E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5257e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.269           19.13       0.0053306       -0.012395
v  Velocity[Y]             -15.577          15.242         0.35137         0.52236
v  Velocity[Z]             -25.331          11.655         -1.6409        -0.50615
v  ǁVelocityǁ         0.00041899          25.731          7.6118          6.5021
v  Pressure                -508.65           171.9         -2.8014          2.7788
v  k                   9.7265e-011          8.5394         0.25683         0.55561
v  omega                    57.499     2.7319e+008     1.2912e+006           76838
v  TempK                    298.53          363.17          338.39          347.65
v  TurbVisc            2.4373e-018       0.0021855     6.6376e-005      0.00023287
v  CourantNb            0.00019768          1.5324         0.78783          0.9693
v  FourierNb             0.0037902               1         0.42488          0.1955
v  total_pressure      1.0082e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0036412     7.4298e-005      0.00020263

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.55          306.63
v  Yplus               0          2.9188         0.62702         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5281          2.1396          1.2127          1.1648


 INSTANT    0.979000000E-02   TIME STEP NUMBER             979
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925325E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10809E-01 0.46927E+01
   Friction velocity        uk    :  0.10809E-01 0.46887E+01
   Dimensionless distance   yplus :  0.73285E-02 0.29184E+01
   Friction thermal sca.    tstar :  0.12095E+01 0.23948E+03
   Rough dim-less th. sca.  tplus :  0.51915E-02 0.20674E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26856E+00      11   0.18224E-04   0.60804E+01 0.38959E+02 
c  Velocity[X]                                      0.25290E+01 
c  Velocity[Y]                                      0.16743E+01 
c  Velocity[Z]                                      0.18771E+01 
c  Pressure     0.18758E-04      18   0.34404E-03   0.19626E-01 0.13574E+02 
c  k            0.21160E-01      13   0.91674E-04   0.23574E+00 0.63142E+02 
c  omega        0.27922E+07       1   0.10237E-06   0.19466E+08 0.72545E+00 
c  TempK        0.10049E+05       4   0.46918E-05   0.53883E+01 0.81238E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5213e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.267          19.131       0.0054706       -0.012303
v  Velocity[Y]             -15.672          15.249         0.35196         0.52319
v  Velocity[Z]             -25.335          11.653         -1.6411        -0.50618
v  ǁVelocityǁ         0.00041869          25.734          7.6117          6.5023
v  Pressure                -509.01          171.88          -2.819          2.7601
v  k                   9.7265e-011           8.314         0.25686         0.55556
v  omega                    57.499     2.7319e+008     1.2912e+006           76838
v  TempK                    298.53          363.17          338.39          347.66
v  TurbVisc            2.4373e-018       0.0021694     6.6378e-005      0.00023286
v  CourantNb            0.00020124          1.5334         0.78784         0.96931
v  FourierNb               0.00379               1         0.42488         0.19546
v  total_pressure      1.0082e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0037015     7.4293e-005       0.0002026

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.55          306.63
v  Yplus               0          2.9184         0.62704         0.48194


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62398          2.1408          1.2127          1.1648


 INSTANT    0.980000000E-02   TIME STEP NUMBER             980
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925120E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10868E-01 0.46927E+01
   Friction velocity        uk    :  0.10868E-01 0.46887E+01
   Dimensionless distance   yplus :  0.73685E-02 0.29180E+01
   Friction thermal sca.    tstar :  0.12096E+01 0.23818E+03
   Rough dim-less th. sca.  tplus :  0.52199E-02 0.20671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26856E+00      11   0.17917E-04   0.60639E+01 0.38961E+02 
c  Velocity[X]                                      0.25248E+01 
c  Velocity[Y]                                      0.16716E+01 
c  Velocity[Z]                                      0.18675E+01 
c  Pressure     0.18436E-04      17   0.34276E-03   0.19290E-01 0.13180E+02 
c  k            0.21159E-01      13   0.91252E-04   0.23518E+00 0.63139E+02 
c  omega        0.27922E+07       1   0.10280E-06   0.20105E+08 0.73543E+00 
c  TempK        0.10049E+05       4   0.46888E-05   0.53980E+01 0.81318E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5168e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.266          19.132       0.0056084       -0.012218
v  Velocity[Y]              -15.76          15.257         0.35255         0.52401
v  Velocity[Z]             -25.338          11.651         -1.6412         -0.5062
v  ǁVelocityǁ         0.00041879          25.736          7.6117          6.5025
v  Pressure                -508.77          171.86         -2.8325          2.7459
v  k                   9.7266e-011          7.9679         0.25689         0.55551
v  omega                    57.499     2.7319e+008     1.2912e+006           76837
v  TempK                    298.53          363.17          338.39          347.66
v  TurbVisc            2.4373e-018       0.0021515     6.6379e-005      0.00023284
v  CourantNb            0.00018258          1.5345         0.78785         0.96933
v  FourierNb             0.0037899               1         0.42488         0.19542
v  total_pressure      1.0082e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0037501     7.4289e-005      0.00020258

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.55          306.63
v  Yplus               0           2.918         0.62705         0.48194


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59343          2.1419          1.2127          1.1648


 INSTANT    0.981000000E-02   TIME STEP NUMBER             981
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925151E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10851E-01 0.46926E+01
   Friction velocity        uk    :  0.10851E-01 0.46886E+01
   Dimensionless distance   yplus :  0.73575E-02 0.29176E+01
   Friction thermal sca.    tstar :  0.12100E+01 0.23854E+03
   Rough dim-less th. sca.  tplus :  0.52121E-02 0.20668E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26856E+00      11   0.17817E-04   0.60448E+01 0.38942E+02 
c  Velocity[X]                                      0.25188E+01 
c  Velocity[Y]                                      0.16676E+01 
c  Velocity[Z]                                      0.18584E+01 
c  Pressure     0.18403E-04      18   0.34753E-03   0.19257E-01 0.13272E+02 
c  k            0.21158E-01      13   0.90556E-04   0.23448E+00 0.63118E+02 
c  omega        0.27922E+07       1   0.10319E-06   0.23842E+08 0.79693E+00 
c  TempK        0.10049E+05       4   0.46855E-05   0.54001E+01 0.81369E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.513e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.264          19.133       0.0057406       -0.012134
v  Velocity[Y]             -15.743          15.264         0.35314         0.52482
v  Velocity[Z]             -25.341          11.649         -1.6414        -0.50623
v  ǁVelocityǁ         0.00041887          25.739          7.6117          6.5027
v  Pressure                -509.14          171.84         -2.8462           2.732
v  k                   9.7267e-011          7.6421         0.25692         0.55545
v  omega                    57.499     2.7319e+008     1.2912e+006           76837
v  TempK                    298.53          363.17           338.4          347.67
v  TurbVisc            2.4373e-018       0.0021319     6.6378e-005      0.00023283
v  CourantNb             0.0001541          1.5354         0.78785         0.96935
v  FourierNb             0.0037898               1         0.42488         0.19538
v  total_pressure      1.0082e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0037852     7.4286e-005      0.00020256

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.55          306.63
v  Yplus               0          2.9176         0.62706         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47765          2.1429          1.2127          1.1647


 INSTANT    0.982000000E-02   TIME STEP NUMBER             982
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925364E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10838E-01 0.46926E+01
   Friction velocity        uk    :  0.10838E-01 0.46886E+01
   Dimensionless distance   yplus :  0.73481E-02 0.29172E+01
   Friction thermal sca.    tstar :  0.12100E+01 0.23884E+03
   Rough dim-less th. sca.  tplus :  0.52054E-02 0.20665E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26856E+00      11   0.17827E-04   0.60285E+01 0.38903E+02 
c  Velocity[X]                                      0.25136E+01 
c  Velocity[Y]                                      0.16553E+01 
c  Velocity[Z]                                      0.18597E+01 
c  Pressure     0.18359E-04      17   0.34648E-03   0.19211E-01 0.13863E+02 
c  k            0.21158E-01      13   0.89935E-04   0.23356E+00 0.63062E+02 
c  omega        0.27922E+07       1   0.10034E-06   0.13667E+08 0.64289E+00 
c  TempK        0.10050E+05       4   0.46826E-05   0.54016E+01 0.81430E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5092e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.263          19.134       0.0058707       -0.012049
v  Velocity[Y]             -15.664          15.272         0.35373         0.52564
v  Velocity[Z]             -25.344          11.648         -1.6415        -0.50625
v  ǁVelocityǁ         0.00041889          25.742          7.6116          6.5029
v  Pressure                -509.89          171.82         -2.8697          2.7082
v  k                   9.7268e-011          7.5598         0.25695          0.5554
v  omega                    57.499     2.7319e+008     1.2912e+006           76837
v  TempK                    298.53          363.17           338.4          347.68
v  TurbVisc            2.4374e-018       0.0021109     6.6379e-005      0.00023281
v  CourantNb            0.00011481          1.5363         0.78786         0.96937
v  FourierNb             0.0037897               1         0.42488         0.19534
v  total_pressure      1.0082e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0038106     7.4284e-005      0.00020255

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.55          306.63
v  Yplus               0          2.9172         0.62707         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43453          2.1439          1.2127          1.1647


 INSTANT    0.983000000E-02   TIME STEP NUMBER             983
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925053E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10834E-01 0.46926E+01
   Friction velocity        uk    :  0.10834E-01 0.46885E+01
   Dimensionless distance   yplus :  0.73455E-02 0.29167E+01
   Friction thermal sca.    tstar :  0.12095E+01 0.23893E+03
   Rough dim-less th. sca.  tplus :  0.52036E-02 0.20662E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         54 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26855E+00      11   0.17743E-04   0.59920E+01 0.38875E+02 
c  Velocity[X]                                      0.25086E+01 
c  Velocity[Y]                                      0.16464E+01 
c  Velocity[Z]                                      0.18370E+01 
c  Pressure     0.17936E-04      17   0.34020E-03   0.18768E-01 0.13390E+02 
c  k            0.21157E-01      13   0.89336E-04   0.23273E+00 0.63022E+02 
c  omega        0.27922E+07       1   0.99369E-07   0.10206E+08 0.58865E+00 
c  TempK        0.10050E+05       4   0.46792E-05   0.54058E+01 0.81493E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5051e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.261          19.135       0.0060001       -0.011961
v  Velocity[Y]             -15.645          15.279         0.35432         0.52646
v  Velocity[Z]             -25.347          11.646         -1.6416        -0.50628
v  ǁVelocityǁ          0.0004189          25.744          7.6116          6.5031
v  Pressure                 -510.6          171.82         -2.8744           2.703
v  k                   9.7269e-011          7.7451         0.25697         0.55535
v  omega                    57.499     2.7319e+008     1.2912e+006           76837
v  TempK                    298.53          363.17           338.4          347.68
v  TurbVisc            2.4374e-018       0.0020886     6.6377e-005      0.00023279
v  CourantNb            0.00016853          1.5372         0.78787         0.96939
v  FourierNb             0.0037896               1         0.42488         0.19531
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0038296     7.4282e-005      0.00020254

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.55          306.63
v  Yplus               0          2.9167         0.62708         0.48194


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.36628          2.1449          1.2128          1.1647


 INSTANT    0.984000000E-02   TIME STEP NUMBER             984
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924984E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10834E-01 0.46925E+01
   Friction velocity        uk    :  0.10834E-01 0.46885E+01
   Dimensionless distance   yplus :  0.73457E-02 0.29164E+01
   Friction thermal sca.    tstar :  0.12096E+01 0.23892E+03
   Rough dim-less th. sca.  tplus :  0.52037E-02 0.20660E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         55 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26855E+00      11   0.17691E-04   0.59738E+01 0.38856E+02 
c  Velocity[X]                                      0.25063E+01 
c  Velocity[Y]                                      0.16389E+01 
c  Velocity[Z]                                      0.18286E+01 
c  Pressure     0.18012E-04      17   0.34977E-03   0.18849E-01 0.13405E+02 
c  k            0.21157E-01      13   0.88669E-04   0.23179E+00 0.62968E+02 
c  omega        0.27922E+07       1   0.99797E-07   0.10195E+08 0.59814E+00 
c  TempK        0.10050E+05       4   0.46763E-05   0.54097E+01 0.81545E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.5007e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.26          19.136       0.0061278       -0.011874
v  Velocity[Y]             -15.679          15.287         0.35491         0.52728
v  Velocity[Z]              -25.35          11.645         -1.6418         -0.5063
v  ǁVelocityǁ         0.00041907          25.747          7.6116          6.5032
v  Pressure                -511.24          171.82         -2.8789          2.6984
v  k                    9.727e-011           8.053           0.257         0.55531
v  omega                    57.498     2.7319e+008     1.2912e+006           76837
v  TempK                    298.53          363.17          338.41          347.69
v  TurbVisc            2.4374e-018        0.002089     6.6375e-005      0.00023277
v  CourantNb             0.0002371          1.5383         0.78788         0.96941
v  FourierNb             0.0037895               1         0.42488         0.19527
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0038442     7.4281e-005      0.00020253

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.55          306.63
v  Yplus               0          2.9164         0.62709         0.48194


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43203           2.146          1.2128          1.1647


 INSTANT    0.985000000E-02   TIME STEP NUMBER             985
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484925098E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10805E-01 0.46925E+01
   Friction velocity        uk    :  0.10805E-01 0.46885E+01
   Dimensionless distance   yplus :  0.73260E-02 0.29166E+01
   Friction thermal sca.    tstar :  0.12096E+01 0.23956E+03
   Rough dim-less th. sca.  tplus :  0.51898E-02 0.20661E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26855E+00      11   0.17509E-04   0.59483E+01 0.38833E+02 
c  Velocity[X]                                      0.25030E+01 
c  Velocity[Y]                                      0.16315E+01 
c  Velocity[Z]                                      0.18138E+01 
c  Pressure     0.17753E-04      17   0.34060E-03   0.18578E-01 0.13437E+02 
c  k            0.21156E-01      13   0.88019E-04   0.23073E+00 0.62910E+02 
c  omega        0.27922E+07       1   0.10297E-06   0.17373E+08 0.72202E+00 
c  TempK        0.10050E+05       4   0.46733E-05   0.54189E+01 0.81621E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4958e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.259          19.137       0.0062525       -0.011791
v  Velocity[Y]             -15.761          15.295          0.3555         0.52809
v  Velocity[Z]             -25.354          11.731         -1.6419        -0.50633
v  ǁVelocityǁ         0.00041896           25.75          7.6116          6.5034
v  Pressure                -511.44          171.82         -2.8811           2.695
v  k                   9.7271e-011          7.9043         0.25703         0.55527
v  omega                    57.498     2.7319e+008     1.2912e+006           76837
v  TempK                    298.53          363.17          338.41          347.69
v  TurbVisc            2.4374e-018       0.0020901     6.6373e-005      0.00023275
v  CourantNb              0.000183          1.5394         0.78789         0.96943
v  FourierNb             0.0037894               1         0.42488         0.19524
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0038553      7.428e-005      0.00020253

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.55          306.63
v  Yplus               0          2.9166          0.6271         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40253          2.1473          1.2128          1.1647


 INSTANT    0.986000000E-02   TIME STEP NUMBER             986
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924963E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10828E-01 0.46924E+01
   Friction velocity        uk    :  0.10828E-01 0.46884E+01
   Dimensionless distance   yplus :  0.73414E-02 0.29167E+01
   Friction thermal sca.    tstar :  0.12097E+01 0.23906E+03
   Rough dim-less th. sca.  tplus :  0.52007E-02 0.20662E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26854E+00      11   0.17467E-04   0.59349E+01 0.38849E+02 
c  Velocity[X]                                      0.24995E+01 
c  Velocity[Y]                                      0.16308E+01 
c  Velocity[Z]                                      0.18046E+01 
c  Pressure     0.17798E-04      17   0.34129E-03   0.18624E-01 0.13416E+02 
c  k            0.21156E-01      13   0.87148E-04   0.22947E+00 0.62833E+02 
c  omega        0.27922E+07       1   0.10532E-06   0.21957E+08 0.79317E+00 
c  TempK        0.10051E+05       4   0.46707E-05   0.54300E+01 0.81698E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4908e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.138       0.0063766       -0.011704
v  Velocity[Y]             -15.833          15.303         0.35609         0.52891
v  Velocity[Z]             -25.357          12.404         -1.6421        -0.50636
v  ǁVelocityǁ         0.00038573          25.753          7.6116          6.5035
v  Pressure                -511.08          171.83          -2.879          2.6958
v  k                   9.7272e-011          7.6897         0.25706         0.55523
v  omega                    57.498     2.7319e+008     1.2912e+006           76837
v  TempK                    298.53          363.17          338.41           347.7
v  TurbVisc            2.4375e-018        0.002092     6.6371e-005      0.00023273
v  CourantNb            8.947e-005          1.5406          0.7879         0.96945
v  FourierNb             0.0037893               1         0.42488          0.1952
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0038672     7.4279e-005      0.00020252

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.55          306.63
v  Yplus               0          2.9167         0.62712         0.48194


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.37416          2.1485          1.2128          1.1647


 INSTANT    0.987000000E-02   TIME STEP NUMBER             987
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924713E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.35021E-02 0.46924E+01
   Friction velocity        uk    :  0.35019E-02 0.46884E+01
   Dimensionless distance   yplus :  0.25111E-02 0.29168E+01
   Friction thermal sca.    tstar :  0.12101E+01 0.82603E+03
   Rough dim-less th. sca.  tplus :  0.17789E-02 0.20663E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26854E+00      11   0.17431E-04   0.59154E+01 0.38825E+02 
c  Velocity[X]                                      0.24962E+01 
c  Velocity[Y]                                      0.16259E+01 
c  Velocity[Z]                                      0.17933E+01 
c  Pressure     0.17765E-04      17   0.33958E-03   0.18589E-01 0.13214E+02 
c  k            0.21156E-01      13   0.86120E-04   0.22819E+00 0.62738E+02 
c  omega        0.27922E+07       1   0.10497E-06   0.21733E+08 0.79424E+00 
c  TempK        0.10051E+05       4   0.46675E-05   0.54269E+01 0.81681E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4864e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.139       0.0064991       -0.011613
v  Velocity[Y]             -15.804          15.311         0.35669         0.52973
v  Velocity[Z]              -25.36          12.938         -1.6422         -0.5064
v  ǁVelocityǁ         0.00041894          25.755          7.6116          6.5037
v  Pressure                -511.37          171.83         -2.8775          2.6963
v  k                   9.7274e-011           7.353         0.25709         0.55519
v  omega                    57.498     2.7319e+008     1.2912e+006           76837
v  TempK                    298.53          363.17          338.42          347.71
v  TurbVisc            2.4375e-018        0.002096      6.637e-005      0.00023271
v  CourantNb           5.9344e-005          1.5417         0.78791         0.96948
v  FourierNb             0.0037892               1         0.42487         0.19516
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0038793     7.4279e-005      0.00020251

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.55          306.63
v  Yplus               0          2.9168         0.62713         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45425          2.1497          1.2128          1.1646


 INSTANT    0.988000000E-02   TIME STEP NUMBER             988
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924628E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10834E-01 0.46923E+01
   Friction velocity        uk    :  0.10834E-01 0.46883E+01
   Dimensionless distance   yplus :  0.73456E-02 0.29169E+01
   Friction thermal sca.    tstar :  0.12101E+01 0.23892E+03
   Rough dim-less th. sca.  tplus :  0.52037E-02 0.20663E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26854E+00      11   0.17366E-04   0.58847E+01 0.38731E+02 
c  Velocity[X]                                      0.24920E+01 
c  Velocity[Y]                                      0.16122E+01 
c  Velocity[Z]                                      0.17805E+01 
c  Pressure     0.17760E-04      17   0.33327E-03   0.18584E-01 0.13132E+02 
c  k            0.21156E-01      13   0.85135E-04   0.22684E+00 0.62606E+02 
c  omega        0.27922E+07       1   0.10332E-06   0.16109E+08 0.71785E+00 
c  TempK        0.10051E+05       4   0.46645E-05   0.54224E+01 0.81678E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4819e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255           19.14       0.0066237       -0.011516
v  Velocity[Y]             -15.713          15.319         0.35729         0.53055
v  Velocity[Z]             -25.363          13.213         -1.6423        -0.50644
v  ǁVelocityǁ          0.0004191          25.758          7.6116          6.5038
v  Pressure                -512.04          171.84         -2.8773          2.6964
v  k                   9.7275e-011          7.1352         0.25711         0.55516
v  omega                    57.498     2.7319e+008     1.2912e+006           76837
v  TempK                    298.53          363.17          338.42          347.71
v  TurbVisc            2.4375e-018       0.0020922     6.6369e-005       0.0002327
v  CourantNb            0.00012127          1.5427         0.78792          0.9695
v  FourierNb             0.0037891               1         0.42487         0.19513
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006        0.003889     7.4279e-005      0.00020251

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.55          306.63
v  Yplus               0          2.9169         0.62714         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46816          2.1508          1.2128          1.1646


 INSTANT    0.989000000E-02   TIME STEP NUMBER             989
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924625E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10804E-01 0.46922E+01
   Friction velocity        uk    :  0.10804E-01 0.46882E+01
   Dimensionless distance   yplus :  0.73251E-02 0.29170E+01
   Friction thermal sca.    tstar :  0.12096E+01 0.23959E+03
   Rough dim-less th. sca.  tplus :  0.51891E-02 0.20664E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         54 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26853E+00      11   0.17342E-04   0.58676E+01 0.38689E+02 
c  Velocity[X]                                      0.24927E+01 
c  Velocity[Y]                                      0.16040E+01 
c  Velocity[Z]                                      0.17709E+01 
c  Pressure     0.17802E-04      17   0.33038E-03   0.18628E-01 0.13229E+02 
c  k            0.21157E-01      13   0.84239E-04   0.22552E+00 0.62479E+02 
c  omega        0.27922E+07       1   0.10185E-06   0.11044E+08 0.63561E+00 
c  TempK        0.10051E+05       4   0.46617E-05   0.54243E+01 0.81692E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4773e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.254          19.141       0.0067524       -0.011418
v  Velocity[Y]             -15.689          15.327         0.35789         0.53137
v  Velocity[Z]             -25.366          13.049         -1.6424        -0.50648
v  ǁVelocityǁ         0.00041909          25.761          7.6116           6.504
v  Pressure                -512.69          171.84          -2.876          2.6973
v  k                   9.7276e-011          7.0428         0.25714         0.55514
v  omega                    57.498     2.7319e+008     1.2912e+006           76837
v  TempK                    298.53          363.17          338.42          347.72
v  TurbVisc            2.4376e-018       0.0020903     6.6369e-005      0.00023269
v  CourantNb            0.00010041          1.5439         0.78793         0.96953
v  FourierNb              0.003789               1         0.42487          0.1951
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0039638     7.4279e-005      0.00020251

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.63
v  Yplus               0           2.917         0.62715         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63436           2.152          1.2128          1.1646


 INSTANT    0.990000000E-02   TIME STEP NUMBER             990
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924569E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10810E-01 0.46922E+01
   Friction velocity        uk    :  0.10810E-01 0.46882E+01
   Dimensionless distance   yplus :  0.73293E-02 0.29171E+01
   Friction thermal sca.    tstar :  0.12097E+01 0.23945E+03
   Rough dim-less th. sca.  tplus :  0.51921E-02 0.20665E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         54 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26853E+00      11   0.17360E-04   0.58536E+01 0.38657E+02 
c  Velocity[X]                                      0.24927E+01 
c  Velocity[Y]                                      0.15975E+01 
c  Velocity[Z]                                      0.17634E+01 
c  Pressure     0.17779E-04      17   0.32969E-03   0.18605E-01 0.13243E+02 
c  k            0.21158E-01      13   0.83522E-04   0.22422E+00 0.62354E+02 
c  omega        0.27922E+07       1   0.10166E-06   0.10330E+08 0.62196E+00 
c  TempK        0.10051E+05       4   0.46587E-05   0.54241E+01 0.81707E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4723e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.141       0.0068813       -0.011318
v  Velocity[Y]             -15.722          15.336         0.35849         0.53219
v  Velocity[Z]             -25.369          12.407         -1.6425        -0.50652
v  ǁVelocityǁ         0.00041919          25.763          7.6116          6.5041
v  Pressure                -513.25          171.85         -2.8718          2.7016
v  k                   9.7277e-011          6.9949         0.25717         0.55511
v  omega                    57.498     2.7319e+008     1.2912e+006           76837
v  TempK                    298.53          363.17          338.43          347.72
v  TurbVisc            2.4376e-018       0.0020872     6.6368e-005      0.00023267
v  CourantNb            7.043e-005          1.5451         0.78794         0.96956
v  FourierNb              0.003789               1         0.42486         0.19506
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0043602     7.4278e-005      0.00020251

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.63
v  Yplus               0          2.9171         0.62716         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53525          2.1532          1.2128          1.1646


 INSTANT    0.991000000E-02   TIME STEP NUMBER             991
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924465E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10792E-01 0.46921E+01
   Friction velocity        uk    :  0.10792E-01 0.46881E+01
   Dimensionless distance   yplus :  0.73174E-02 0.29172E+01
   Friction thermal sca.    tstar :  0.12098E+01 0.23985E+03
   Rough dim-less th. sca.  tplus :  0.51837E-02 0.20665E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26853E+00      11   0.17313E-04   0.58409E+01 0.38631E+02 
c  Velocity[X]                                      0.24937E+01 
c  Velocity[Y]                                      0.15919E+01 
c  Velocity[Z]                                      0.17552E+01 
c  Pressure     0.17767E-04      17   0.33068E-03   0.18594E-01 0.13224E+02 
c  k            0.21159E-01      13   0.82601E-04   0.22288E+00 0.62224E+02 
c  omega        0.27922E+07       1   0.10401E-06   0.15559E+08 0.70830E+00 
c  TempK        0.10052E+05       4   0.46555E-05   0.54270E+01 0.81742E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4668e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.252          19.142       0.0070096       -0.011221
v  Velocity[Y]             -15.784          15.344         0.35908         0.53302
v  Velocity[Z]             -25.373          11.635         -1.6426        -0.50656
v  ǁVelocityǁ         0.00041917          25.766          7.6116          6.5042
v  Pressure                -513.69          171.86         -2.8631          2.7094
v  k                   9.7279e-011          6.9088          0.2572         0.55509
v  omega                    57.498     2.7319e+008     1.2912e+006           76837
v  TempK                    298.53          363.17          338.43          347.73
v  TurbVisc            2.4376e-018       0.0020925     6.6368e-005      0.00023267
v  CourantNb           8.5919e-005          1.5464         0.78795         0.96958
v  FourierNb             0.0037889               1         0.42486         0.19503
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0047721     7.4279e-005       0.0002025

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.63
v  Yplus               0          2.9172         0.62718         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62788          2.1546          1.2128          1.1646


 INSTANT    0.992000000E-02   TIME STEP NUMBER             992
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924230E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10799E-01 0.46920E+01
   Friction velocity        uk    :  0.10799E-01 0.46880E+01
   Dimensionless distance   yplus :  0.73217E-02 0.29172E+01
   Friction thermal sca.    tstar :  0.12098E+01 0.23971E+03
   Rough dim-less th. sca.  tplus :  0.51867E-02 0.20666E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26852E+00      11   0.17258E-04   0.58430E+01 0.38661E+02 
c  Velocity[X]                                      0.24976E+01 
c  Velocity[Y]                                      0.15898E+01 
c  Velocity[Z]                                      0.17556E+01 
c  Pressure     0.17968E-04      18   0.32843E-03   0.18803E-01 0.13778E+02 
c  k            0.21160E-01      13   0.81628E-04   0.22155E+00 0.62096E+02 
c  omega        0.27922E+07       1   0.10775E-06   0.23369E+08 0.81840E+00 
c  TempK        0.10052E+05       4   0.46526E-05   0.54305E+01 0.81799E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4611e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.251          19.143       0.0071384        -0.01112
v  Velocity[Y]             -15.911          15.352         0.35968         0.53384
v  Velocity[Z]             -25.376          11.633         -1.6427         -0.5066
v  ǁVelocityǁ         0.00041908          25.769          7.6115          6.5044
v  Pressure                -513.02          171.89         -2.8399          2.7312
v  k                    9.728e-011          6.6972         0.25722         0.55507
v  omega                    57.498     2.7319e+008     1.2912e+006           76836
v  TempK                    298.53          363.17          338.43          347.74
v  TurbVisc            2.4377e-018       0.0021014     6.6368e-005      0.00023266
v  CourantNb            0.00012198          1.5477         0.78796         0.96961
v  FourierNb             0.0037888               1         0.42486           0.195
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006        0.004462     7.4279e-005       0.0002025

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.63
v  Yplus               0          2.9172         0.62719         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41149           2.156          1.2128          1.1646


 INSTANT    0.993000000E-02   TIME STEP NUMBER             993
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924083E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10815E-01 0.46919E+01
   Friction velocity        uk    :  0.10815E-01 0.46879E+01
   Dimensionless distance   yplus :  0.73324E-02 0.29173E+01
   Friction thermal sca.    tstar :  0.12103E+01 0.23935E+03
   Rough dim-less th. sca.  tplus :  0.51944E-02 0.20666E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26852E+00      11   0.17205E-04   0.58416E+01 0.38713E+02 
c  Velocity[X]                                      0.24991E+01 
c  Velocity[Y]                                      0.15950E+01 
c  Velocity[Z]                                      0.17474E+01 
c  Pressure     0.18154E-04      17   0.33106E-03   0.18998E-01 0.13363E+02 
c  k            0.21161E-01      13   0.80662E-04   0.22025E+00 0.61975E+02 
c  omega        0.27922E+07       1   0.10780E-06   0.24696E+08 0.83830E+00 
c  TempK        0.10052E+05       4   0.46490E-05   0.54306E+01 0.81818E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4561e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.25          19.143       0.0072666       -0.011017
v  Velocity[Y]             -15.844          15.361         0.36027         0.53466
v  Velocity[Z]             -25.379          11.632         -1.6428        -0.50663
v  ǁVelocityǁ         0.00041902          25.772          7.6115          6.5045
v  Pressure                -513.52           171.9         -2.8258          2.7442
v  k                   9.7281e-011          6.2838         0.25725         0.55506
v  omega                    57.498     2.7319e+008     1.2912e+006           76836
v  TempK                    298.54          363.17          338.44          347.74
v  TurbVisc            2.4377e-018       0.0021081     6.6368e-005      0.00023265
v  CourantNb            0.00017387          1.5489         0.78797         0.96963
v  FourierNb             0.0037888               1         0.42486         0.19497
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0039243      7.428e-005      0.00020249

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.63
v  Yplus               0          2.9173         0.62721         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45191          2.1572          1.2128          1.1646


 INSTANT    0.994000000E-02   TIME STEP NUMBER             994
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924154E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10830E-01 0.46918E+01
   Friction velocity        uk    :  0.10830E-01 0.46878E+01
   Dimensionless distance   yplus :  0.73429E-02 0.29174E+01
   Friction thermal sca.    tstar :  0.12102E+01 0.23901E+03
   Rough dim-less th. sca.  tplus :  0.52017E-02 0.20667E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         54 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26851E+00      11   0.17195E-04   0.58275E+01 0.38636E+02 
c  Velocity[X]                                      0.25013E+01 
c  Velocity[Y]                                      0.15829E+01 
c  Velocity[Z]                                      0.17433E+01 
c  Pressure     0.17889E-04      17   0.33226E-03   0.18720E-01 0.13112E+02 
c  k            0.21163E-01      13   0.79796E-04   0.21880E+00 0.61822E+02 
c  omega        0.27922E+07       1   0.10607E-06   0.20639E+08 0.78426E+00 
c  TempK        0.10052E+05       4   0.46452E-05   0.54318E+01 0.81828E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4511e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.249          19.144       0.0073942       -0.010911
v  Velocity[Y]             -15.776          15.369         0.36086         0.53548
v  Velocity[Z]             -25.382          11.705         -1.6429        -0.50667
v  ǁVelocityǁ         0.00041923          25.774          7.6115          6.5046
v  Pressure                -514.36          171.91         -2.8189          2.7509
v  k                   9.7282e-011          6.2459         0.25727         0.55504
v  omega                    57.497     2.7319e+008     1.2912e+006           76836
v  TempK                    298.54          363.17          338.44          347.75
v  TurbVisc            2.4377e-018       0.0021124     6.6367e-005      0.00023265
v  CourantNb            0.00021515          1.5501         0.78798         0.96965
v  FourierNb             0.0037887               1         0.42486         0.19493
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0037013     7.4279e-005      0.00020249

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.63
v  Yplus               0          2.9174         0.62722         0.48194


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52987          2.1585          1.2128          1.1646


 INSTANT    0.995000000E-02   TIME STEP NUMBER             995
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924271E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10789E-01 0.46918E+01
   Friction velocity        uk    :  0.10788E-01 0.46877E+01
   Dimensionless distance   yplus :  0.73148E-02 0.29174E+01
   Friction thermal sca.    tstar :  0.12097E+01 0.23993E+03
   Rough dim-less th. sca.  tplus :  0.51818E-02 0.20667E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         55 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26851E+00      11   0.17117E-04   0.58187E+01 0.38612E+02 
c  Velocity[X]                                      0.25021E+01 
c  Velocity[Y]                                      0.15776E+01 
c  Velocity[Z]                                      0.17391E+01 
c  Pressure     0.17671E-04      17   0.32849E-03   0.18492E-01 0.13113E+02 
c  k            0.21165E-01      13   0.78808E-04   0.21729E+00 0.61649E+02 
c  omega        0.27922E+07       1   0.10235E-06   0.11139E+08 0.63414E+00 
c  TempK        0.10052E+05       4   0.46407E-05   0.54320E+01 0.81859E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4457e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.249          19.144        0.007519       -0.010804
v  Velocity[Y]             -15.752          15.378         0.36145          0.5363
v  Velocity[Z]             -25.385          12.069          -1.643         -0.5067
v  ǁVelocityǁ          0.0004192          25.777          7.6115          6.5048
v  Pressure                -515.05          171.92         -2.8093          2.7598
v  k                   9.7283e-011          6.2592          0.2573         0.55502
v  omega                    57.497     2.7319e+008     1.2912e+006           76836
v  TempK                    298.54          363.17          338.44          347.75
v  TurbVisc            2.4377e-018       0.0021143     6.6367e-005      0.00023264
v  CourantNb            0.00021518          1.5514         0.78799         0.96967
v  FourierNb             0.0037887               1         0.42486          0.1949
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0035043      7.428e-005      0.00020249

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.63
v  Yplus               0          2.9174         0.62723         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63397          2.1598          1.2128          1.1646


 INSTANT    0.996000000E-02   TIME STEP NUMBER             996
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924167E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10796E-01 0.46917E+01
   Friction velocity        uk    :  0.10796E-01 0.46877E+01
   Dimensionless distance   yplus :  0.73200E-02 0.29175E+01
   Friction thermal sca.    tstar :  0.12098E+01 0.23976E+03
   Rough dim-less th. sca.  tplus :  0.51855E-02 0.20668E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         55 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26850E+00      11   0.17042E-04   0.58130E+01 0.38607E+02 
c  Velocity[X]                                      0.25030E+01 
c  Velocity[Y]                                      0.15728E+01 
c  Velocity[Z]                                      0.17373E+01 
c  Pressure     0.17508E-04      17   0.32652E-03   0.18320E-01 0.13137E+02 
c  k            0.21167E-01      13   0.77854E-04   0.21569E+00 0.61474E+02 
c  omega        0.27922E+07       1   0.10191E-06   0.10468E+08 0.62370E+00 
c  TempK        0.10053E+05       4   0.46362E-05   0.54342E+01 0.81895E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step       6.44e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.248          19.145       0.0076438         -0.0107
v  Velocity[Y]             -15.773          15.386         0.36204         0.53713
v  Velocity[Z]             -25.388          13.411          -1.643        -0.50673
v  ǁVelocityǁ          0.0003997           25.78          7.6115          6.5049
v  Pressure                -515.76          171.95         -2.7917          2.7765
v  k                   9.7285e-011          6.2815         0.25732         0.55501
v  omega                    57.497     2.7319e+008     1.2912e+006           76836
v  TempK                    298.54          363.17          338.45          347.76
v  TurbVisc            2.4378e-018       0.0021161     6.6366e-005      0.00023264
v  CourantNb            0.00023149          1.5528           0.788         0.96969
v  FourierNb             0.0037886               1         0.42485         0.19487
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0036379     7.4281e-005      0.00020249

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.63
v  Yplus               0          2.9175         0.62724         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52512          2.1612          1.2129          1.1646


 INSTANT    0.997000000E-02   TIME STEP NUMBER             997
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924075E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10779E-01 0.46916E+01
   Friction velocity        uk    :  0.10778E-01 0.46876E+01
   Dimensionless distance   yplus :  0.73080E-02 0.29175E+01
   Friction thermal sca.    tstar :  0.12098E+01 0.24015E+03
   Rough dim-less th. sca.  tplus :  0.51770E-02 0.20668E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         55 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26850E+00      11   0.17026E-04   0.58084E+01 0.38603E+02 
c  Velocity[X]                                      0.25066E+01 
c  Velocity[Y]                                      0.15672E+01 
c  Velocity[Z]                                      0.17346E+01 
c  Pressure     0.17422E-04      18   0.32204E-03   0.18230E-01 0.13279E+02 
c  k            0.21169E-01      13   0.76939E-04   0.21396E+00 0.61290E+02 
c  omega        0.27922E+07       1   0.10173E-06   0.10265E+08 0.61693E+00 
c  TempK        0.10053E+05       4   0.46319E-05   0.54352E+01 0.81930E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4337e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.248          19.145       0.0077701       -0.010595
v  Velocity[Y]             -15.805          15.395         0.36263         0.53796
v  Velocity[Z]             -25.392          14.198         -1.6431        -0.50677
v  ǁVelocityǁ         0.00035044          25.783          7.6116           6.505
v  Pressure                -516.59          171.96         -2.7744          2.7931
v  k                   9.7286e-011          6.3101         0.25734         0.55499
v  omega                    57.497     2.7318e+008     1.2912e+006           76836
v  TempK                    298.54          363.17          338.45          347.77
v  TurbVisc            2.4378e-018       0.0021173     6.6365e-005      0.00023263
v  CourantNb             0.0002436          1.5543         0.78801          0.9697
v  FourierNb             0.0037886               1         0.42485         0.19485
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0036568     7.4282e-005      0.00020249

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.63
v  Yplus               0          2.9175         0.62725         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58289          2.1628          1.2129          1.1646


 INSTANT    0.998000000E-02   TIME STEP NUMBER             998
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923990E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10780E-01 0.46915E+01
   Friction velocity        uk    :  0.10780E-01 0.46875E+01
   Dimensionless distance   yplus :  0.73088E-02 0.29176E+01
   Friction thermal sca.    tstar :  0.12098E+01 0.24013E+03
   Rough dim-less th. sca.  tplus :  0.51776E-02 0.20668E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26850E+00      11   0.16989E-04   0.58112E+01 0.38634E+02 
c  Velocity[X]                                      0.25112E+01 
c  Velocity[Y]                                      0.15632E+01 
c  Velocity[Z]                                      0.17368E+01 
c  Pressure     0.17566E-04      18   0.32128E-03   0.18380E-01 0.13561E+02 
c  k            0.21171E-01      13   0.75818E-04   0.21236E+00 0.61113E+02 
c  omega        0.27922E+07       1   0.10421E-06   0.16984E+08 0.71951E+00 
c  TempK        0.10053E+05       4   0.46273E-05   0.54335E+01 0.81962E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4271e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.247          19.145       0.0078981       -0.010488
v  Velocity[Y]             -15.876          15.403         0.36322         0.53879
v  Velocity[Z]             -25.395          14.221         -1.6432        -0.50681
v  ǁVelocityǁ         0.00030121          25.786          7.6116          6.5051
v  Pressure                -516.91          171.99         -2.7494          2.8168
v  k                   9.7287e-011          6.3376         0.25736         0.55497
v  omega                    57.497     2.7318e+008     1.2912e+006           76836
v  TempK                    298.54          363.17          338.45          347.77
v  TurbVisc            2.4378e-018       0.0021143     6.6363e-005      0.00023263
v  CourantNb            0.00024358          1.5559         0.78801         0.96972
v  FourierNb             0.0037886               1         0.42485         0.19482
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0036302     7.4284e-005      0.00020249

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.64
v  Yplus               0          2.9176         0.62727         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58236          2.1644          1.2129          1.1645


 INSTANT    0.999000000E-02   TIME STEP NUMBER             999
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924008E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10795E-01 0.46914E+01
   Friction velocity        uk    :  0.10795E-01 0.46874E+01
   Dimensionless distance   yplus :  0.73190E-02 0.29176E+01
   Friction thermal sca.    tstar :  0.12099E+01 0.23979E+03
   Rough dim-less th. sca.  tplus :  0.51848E-02 0.20669E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26849E+00      11   0.16973E-04   0.58232E+01 0.38711E+02 
c  Velocity[X]                                      0.25168E+01 
c  Velocity[Y]                                      0.15678E+01 
c  Velocity[Z]                                      0.17387E+01 
c  Pressure     0.17538E-04      17   0.32135E-03   0.18351E-01 0.13850E+02 
c  k            0.21173E-01      13   0.74869E-04   0.21084E+00 0.60943E+02 
c  omega        0.27922E+07       1   0.10728E-06   0.27719E+08 0.86523E+00 
c  TempK        0.10053E+05       4   0.46227E-05   0.54409E+01 0.82009E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4204e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.247          19.146       0.0080292        -0.01038
v  Velocity[Y]             -15.955          15.411         0.36381         0.53963
v  Velocity[Z]             -25.399          13.165         -1.6432        -0.50685
v  ǁVelocityǁ         0.00025415          25.789          7.6116          6.5052
v  Pressure                -516.54          172.02         -2.7217          2.8428
v  k                   9.7288e-011          6.3641         0.25738         0.55496
v  omega                    57.497     2.7318e+008     1.2912e+006           76836
v  TempK                    298.54          363.17          338.46          347.78
v  TurbVisc            2.4379e-018       0.0021101     6.6361e-005      0.00023263
v  CourantNb            0.00024356          1.5575         0.78802         0.96973
v  FourierNb             0.0037885               1         0.42485         0.19479
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0036091     7.4287e-005       0.0002025

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.64
v  Yplus               0          2.9176         0.62729         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66099          2.1661          1.2129          1.1645


 INSTANT    0.100000000E-01   TIME STEP NUMBER            1000
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924078E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10828E-01 0.46914E+01
   Friction velocity        uk    :  0.10828E-01 0.46873E+01
   Dimensionless distance   yplus :  0.73413E-02 0.29177E+01
   Friction thermal sca.    tstar :  0.12102E+01 0.23906E+03
   Rough dim-less th. sca.  tplus :  0.52007E-02 0.20669E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26849E+00      11   0.16885E-04   0.58268E+01 0.38716E+02 
c  Velocity[X]                                      0.25228E+01 
c  Velocity[Y]                                      0.15651E+01 
c  Velocity[Z]                                      0.17389E+01 
c  Pressure     0.17547E-04      17   0.32386E-03   0.18360E-01 0.13213E+02 
c  k            0.21175E-01      13   0.73851E-04   0.20935E+00 0.60781E+02 
c  omega        0.27922E+07       1   0.10490E-06   0.20494E+08 0.76542E+00 
c  TempK        0.10053E+05       4   0.46185E-05   0.54503E+01 0.82022E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4143e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.247          19.146       0.0081593        -0.01027
v  Velocity[Y]             -15.892           15.42          0.3644         0.54047
v  Velocity[Z]             -25.402          13.148         -1.6432         -0.5069
v  ǁVelocityǁ         0.00020969          25.792          7.6116          6.5053
v  Pressure                -517.14          172.03         -2.7064          2.8571
v  k                   9.7289e-011          6.3893          0.2574         0.55494
v  omega                    57.497     2.7318e+008     1.2912e+006           76836
v  TempK                    298.54          363.17          338.46          347.78
v  TurbVisc            2.4379e-018       0.0021047     6.6359e-005      0.00023263
v  CourantNb            0.00024354           1.559         0.78803         0.96974
v  FourierNb             0.0037885               1         0.42484         0.19476
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0035928      7.429e-005      0.00020251

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.64
v  Yplus               0          2.9177          0.6273         0.48192


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49297          2.1675          1.2129          1.1645


 INSTANT    0.100100000E-01   TIME STEP NUMBER            1001
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924188E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10791E-01 0.46913E+01
   Friction velocity        uk    :  0.10791E-01 0.46873E+01
   Dimensionless distance   yplus :  0.73167E-02 0.29177E+01
   Friction thermal sca.    tstar :  0.12102E+01 0.23987E+03
   Rough dim-less th. sca.  tplus :  0.51832E-02 0.20669E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         54 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26848E+00      11   0.16878E-04   0.58268E+01 0.38676E+02 
c  Velocity[X]                                      0.25281E+01 
c  Velocity[Y]                                      0.15574E+01 
c  Velocity[Z]                                      0.17413E+01 
c  Pressure     0.17696E-04      17   0.32403E-03   0.18516E-01 0.13528E+02 
c  k            0.21177E-01      13   0.73018E-04   0.20777E+00 0.60612E+02 
c  omega        0.27922E+07       1   0.10271E-06   0.13352E+08 0.65883E+00 
c  TempK        0.10053E+05       4   0.46155E-05   0.54557E+01 0.82062E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4082e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.246          19.146       0.0082897       -0.010166
v  Velocity[Y]             -15.793          15.428         0.36498         0.54132
v  Velocity[Z]             -25.405          13.276         -1.6433        -0.50694
v  ǁVelocityǁ         0.00016834          25.795          7.6116          6.5055
v  Pressure                -518.01          172.05         -2.6889          2.8738
v  k                    9.729e-011          6.4133         0.25742         0.55493
v  omega                    57.497     2.7318e+008     1.2912e+006           76836
v  TempK                    298.55          363.17          338.46          347.79
v  TurbVisc            2.4379e-018       0.0020979     6.6356e-005      0.00023262
v  CourantNb            0.00024352          1.5605         0.78803         0.96974
v  FourierNb             0.0037885               1         0.42483         0.19473
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0035741     7.4293e-005      0.00020252

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.64
v  Yplus               0          2.9177         0.62731         0.48192


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46617          2.1691          1.2129          1.1645


 INSTANT    0.100200000E-01   TIME STEP NUMBER            1002
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924246E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10799E-01 0.46912E+01
   Friction velocity        uk    :  0.10799E-01 0.46872E+01
   Dimensionless distance   yplus :  0.73217E-02 0.29177E+01
   Friction thermal sca.    tstar :  0.12097E+01 0.23971E+03
   Rough dim-less th. sca.  tplus :  0.51867E-02 0.20669E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         55 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26848E+00      11   0.16841E-04   0.58346E+01 0.38690E+02 
c  Velocity[X]                                      0.25346E+01 
c  Velocity[Y]                                      0.15559E+01 
c  Velocity[Z]                                      0.17440E+01 
c  Pressure     0.17855E-04      18   0.32921E-03   0.18682E-01 0.13799E+02 
c  k            0.21179E-01      13   0.72339E-04   0.20600E+00 0.60428E+02 
c  omega        0.27922E+07       1   0.10223E-06   0.11032E+08 0.62953E+00 
c  TempK        0.10053E+05       4   0.46129E-05   0.54702E+01 0.82140E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.4019e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.246          19.146       0.0084185       -0.010064
v  Velocity[Y]             -15.778          15.436         0.36557         0.54216
v  Velocity[Z]             -25.408          14.166         -1.6433        -0.50699
v  ǁVelocityǁ         0.00013382          25.797          7.6117          6.5056
v  Pressure                -518.63          172.08         -2.6699          2.8917
v  k                   9.7291e-011          6.4357         0.25744         0.55491
v  omega                    57.497     2.7318e+008     1.2912e+006           76836
v  TempK                    298.55          363.17          338.47          347.79
v  TurbVisc            2.4379e-018       0.0020898     6.6353e-005      0.00023262
v  CourantNb             0.0002435           1.562         0.78804         0.96975
v  FourierNb             0.0037885               1         0.42483         0.19471
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006        0.003551     7.4296e-005      0.00020254

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.64
v  Yplus               0          2.9177         0.62733         0.48192


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44995          2.1706          1.2129          1.1645


 INSTANT    0.100300000E-01   TIME STEP NUMBER            1003
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924101E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10790E-01 0.46911E+01
   Friction velocity        uk    :  0.10790E-01 0.46871E+01
   Dimensionless distance   yplus :  0.73161E-02 0.29178E+01
   Friction thermal sca.    tstar :  0.12098E+01 0.23989E+03
   Rough dim-less th. sca.  tplus :  0.51828E-02 0.20670E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         55 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26847E+00      11   0.16881E-04   0.58447E+01 0.38702E+02 
c  Velocity[X]                                      0.25419E+01 
c  Velocity[Y]                                      0.15546E+01 
c  Velocity[Z]                                      0.17481E+01 
c  Pressure     0.18126E-04      18   0.33391E-03   0.18967E-01 0.14393E+02 
c  k            0.21180E-01      13   0.71647E-04   0.20431E+00 0.60245E+02 
c  omega        0.27922E+07       1   0.10292E-06   0.11091E+08 0.64256E+00 
c  TempK        0.10054E+05       4   0.46104E-05   0.54766E+01 0.82207E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3954e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.246          19.146       0.0085448      -0.0099614
v  Velocity[Y]             -15.815          15.444         0.36615         0.54301
v  Velocity[Z]             -25.412          14.282         -1.6433        -0.50703
v  ǁVelocityǁ         0.00011418            25.8          7.6117          6.5057
v  Pressure                -519.23          172.11          -2.639          2.9213
v  k                   9.7292e-011          6.4565         0.25746          0.5549
v  omega                    57.497     2.7318e+008     1.2912e+006           76836
v  TempK                    298.55          363.17          338.47           347.8
v  TurbVisc             2.438e-018       0.0020802     6.6349e-005      0.00023262
v  CourantNb            0.00024348          1.5636         0.78804         0.96976
v  FourierNb             0.0037885               1         0.42482         0.19468
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006        0.003524     7.4299e-005      0.00020255

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.64
v  Yplus               0          2.9178         0.62735         0.48191


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46736          2.1722          1.2129          1.1644


 INSTANT    0.100400000E-01   TIME STEP NUMBER            1004
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924147E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10787E-01 0.46910E+01
   Friction velocity        uk    :  0.10787E-01 0.46870E+01
   Dimensionless distance   yplus :  0.73139E-02 0.29178E+01
   Friction thermal sca.    tstar :  0.12099E+01 0.23996E+03
   Rough dim-less th. sca.  tplus :  0.51812E-02 0.20670E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26847E+00      11   0.16883E-04   0.58571E+01 0.38742E+02 
c  Velocity[X]                                      0.25476E+01 
c  Velocity[Y]                                      0.15524E+01 
c  Velocity[Z]                                      0.17571E+01 
c  Pressure     0.18142E-04      18   0.32808E-03   0.18984E-01 0.14378E+02 
c  k            0.21182E-01      13   0.71318E-04   0.20272E+00 0.60060E+02 
c  omega        0.27922E+07       1   0.10754E-06   0.21531E+08 0.79930E+00 
c  TempK        0.10054E+05       4   0.46090E-05   0.54811E+01 0.82282E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3885e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.246          19.146       0.0086728      -0.0098519
v  Velocity[Y]             -15.967          15.452         0.36674         0.54386
v  Velocity[Z]             -25.415          12.937         -1.6433        -0.50707
v  ǁVelocityǁ         0.00011484          25.803          7.6117          6.5058
v  Pressure                -518.71          172.14         -2.6077          2.9505
v  k                   9.7293e-011          6.4758         0.25747         0.55489
v  omega                    57.497     2.7318e+008     1.2912e+006           76836
v  TempK                    298.55          363.17          338.47           347.8
v  TurbVisc             2.438e-018       0.0020689     6.6347e-005      0.00023262
v  CourantNb            0.00024347          1.5653         0.78805         0.96976
v  FourierNb             0.0037885               1         0.42481         0.19465
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034942       7.43e-005      0.00020256

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.64
v  Yplus               0          2.9178         0.62736         0.48191


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50988          2.1739          1.2129          1.1644


 INSTANT    0.100500000E-01   TIME STEP NUMBER            1005
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923906E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10801E-01 0.46909E+01
   Friction velocity        uk    :  0.10801E-01 0.46869E+01
   Dimensionless distance   yplus :  0.73229E-02 0.29178E+01
   Friction thermal sca.    tstar :  0.12103E+01 0.23966E+03
   Rough dim-less th. sca.  tplus :  0.51876E-02 0.20670E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26846E+00      11   0.16884E-04   0.58789E+01 0.38826E+02 
c  Velocity[X]                                      0.25556E+01 
c  Velocity[Y]                                      0.15597E+01 
c  Velocity[Z]                                      0.17637E+01 
c  Pressure     0.18252E-04      18   0.33911E-03   0.19100E-01 0.15155E+02 
c  k            0.21184E-01      13   0.69973E-04   0.20118E+00 0.59874E+02 
c  omega        0.27922E+07       1   0.10793E-06   0.24801E+08 0.84451E+00 
c  TempK        0.10054E+05       4   0.46089E-05   0.54918E+01 0.82315E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3821e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.247          19.146       0.0088068      -0.0097425
v  Velocity[Y]             -15.962           15.46         0.36733         0.54472
v  Velocity[Z]             -25.418          11.619         -1.6433        -0.50711
v  ǁVelocityǁ         0.00013622          25.806          7.6117           6.506
v  Pressure                -518.56          172.19          -2.567          2.9892
v  k                   9.7294e-011          6.4935         0.25749         0.55487
v  omega                    57.497     2.7318e+008     1.2912e+006           76836
v  TempK                    298.55          363.17          338.48          347.81
v  TurbVisc             2.438e-018       0.0020538     6.6344e-005      0.00023262
v  CourantNb            0.00024345          1.5669         0.78805         0.96977
v  FourierNb             0.0037885               1          0.4248         0.19463
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0038015     7.4302e-005      0.00020257

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.64
v  Yplus               0          2.9178         0.62738          0.4819


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46439          2.1755          1.2129          1.1644


 INSTANT    0.100600000E-01   TIME STEP NUMBER            1006
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923985E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10858E-01 0.46908E+01
   Friction velocity        uk    :  0.10858E-01 0.46868E+01
   Dimensionless distance   yplus :  0.73618E-02 0.29178E+01
   Friction thermal sca.    tstar :  0.12104E+01 0.23840E+03
   Rough dim-less th. sca.  tplus :  0.52152E-02 0.20670E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26846E+00      11   0.16861E-04   0.58831E+01 0.38794E+02 
c  Velocity[X]                                      0.25608E+01 
c  Velocity[Y]                                      0.15535E+01 
c  Velocity[Z]                                      0.17688E+01 
c  Pressure     0.18651E-04      17   0.34216E-03   0.19520E-01 0.13643E+02 
c  k            0.21186E-01      13   0.69178E-04   0.19967E+00 0.59681E+02 
c  omega        0.27922E+07       1   0.10626E-06   0.19768E+08 0.77755E+00 
c  TempK        0.10054E+05       4   0.46091E-05   0.55051E+01 0.82379E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.376e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.247          19.146       0.0089401      -0.0096367
v  Velocity[Y]             -15.921          15.467         0.36791         0.54557
v  Velocity[Z]             -25.421          11.618         -1.6433        -0.50715
v  ǁVelocityǁ         0.00017032          25.808          7.6118          6.5061
v  Pressure                -519.28          172.21         -2.5476          3.0072
v  k                   9.7294e-011          6.5097          0.2575         0.55486
v  omega                    57.497     2.7318e+008     1.2912e+006           76836
v  TempK                    298.55          363.17          338.48          347.82
v  TurbVisc             2.438e-018       0.0020474     6.6341e-005      0.00023262
v  CourantNb            0.00024343          1.5684         0.78806         0.96978
v  FourierNb             0.0037884               1         0.42479          0.1946
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0038675     7.4302e-005      0.00020257

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.64
v  Yplus               0          2.9178         0.62739         0.48189


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52089           2.177          1.2129          1.1644


 INSTANT    0.100700000E-01   TIME STEP NUMBER            1007
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923903E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10824E-01 0.46908E+01
   Friction velocity        uk    :  0.10824E-01 0.46868E+01
   Dimensionless distance   yplus :  0.73387E-02 0.29178E+01
   Friction thermal sca.    tstar :  0.12102E+01 0.23915E+03
   Rough dim-less th. sca.  tplus :  0.51988E-02 0.20670E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         55 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26845E+00      11   0.16817E-04   0.58868E+01 0.38767E+02 
c  Velocity[X]                                      0.25656E+01 
c  Velocity[Y]                                      0.15475E+01 
c  Velocity[Z]                                      0.17737E+01 
c  Pressure     0.18696E-04      17   0.34487E-03   0.19569E-01 0.13906E+02 
c  k            0.21187E-01      13   0.68500E-04   0.19831E+00 0.59492E+02 
c  omega        0.27922E+07       1   0.10404E-06   0.15441E+08 0.70879E+00 
c  TempK        0.10054E+05       4   0.46088E-05   0.55194E+01 0.82468E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3702e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.247          19.147       0.0090734      -0.0095306
v  Velocity[Y]             -15.872          15.475          0.3685         0.54644
v  Velocity[Z]             -25.424          11.617         -1.6433        -0.50719
v  ǁVelocityǁ          0.0002104          25.811          7.6118          6.5063
v  Pressure                -519.71          172.24         -2.5211          3.0325
v  k                   9.7295e-011          6.5244         0.25752         0.55484
v  omega                    57.497     2.7318e+008     1.2912e+006           76836
v  TempK                    298.56          363.17          338.48          347.82
v  TurbVisc            2.4381e-018       0.0020495     6.6339e-005      0.00023263
v  CourantNb            0.00019045          1.5698         0.78807          0.9698
v  FourierNb             0.0037885               1         0.42477         0.19457
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006        0.003827     7.4299e-005      0.00020257

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.56          306.64
v  Yplus               0          2.9178         0.62741         0.48189


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51842          2.1784          1.2128          1.1644


 INSTANT    0.100800000E-01   TIME STEP NUMBER            1008
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924095E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10837E-01 0.46907E+01
   Friction velocity        uk    :  0.10837E-01 0.46867E+01
   Dimensionless distance   yplus :  0.73476E-02 0.29178E+01
   Friction thermal sca.    tstar :  0.12101E+01 0.23886E+03
   Rough dim-less th. sca.  tplus :  0.52051E-02 0.20670E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         55 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26845E+00      11   0.16793E-04   0.58944E+01 0.38771E+02 
c  Velocity[X]                                      0.25687E+01 
c  Velocity[Y]                                      0.15447E+01 
c  Velocity[Z]                                      0.17810E+01 
c  Pressure     0.18696E-04      18   0.36350E-03   0.19572E-01 0.13587E+02 
c  k            0.21188E-01      13   0.67910E-04   0.19716E+00 0.59309E+02 
c  omega        0.27922E+07       1   0.10229E-06   0.10060E+08 0.61453E+00 
c  TempK        0.10054E+05       4   0.46078E-05   0.55311E+01 0.82554E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3642e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.248          19.147       0.0092095      -0.0094225
v  Velocity[Y]             -15.869          15.483         0.36909          0.5473
v  Velocity[Z]             -25.427          11.616         -1.6433        -0.50722
v  ǁVelocityǁ         0.00025511          25.814          7.6119          6.5064
v  Pressure                -520.11          172.27         -2.4978          3.0543
v  k                   9.7296e-011          6.5376         0.25753         0.55482
v  omega                    57.497     2.7317e+008     1.2912e+006           76835
v  TempK                    298.56          363.17          338.49          347.83
v  TurbVisc            2.4381e-018       0.0020515     6.6336e-005      0.00023263
v  CourantNb            0.00012607          1.5713         0.78808         0.96981
v  FourierNb             0.0037885               1         0.42476         0.19454
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0037516     7.4293e-005      0.00020257

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.57          306.64
v  Yplus               0          2.9178         0.62742         0.48188


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53717          2.1799          1.2128          1.1643


 INSTANT    0.100900000E-01   TIME STEP NUMBER            1009
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923886E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10834E-01 0.46906E+01
   Friction velocity        uk    :  0.10834E-01 0.46866E+01
   Dimensionless distance   yplus :  0.73456E-02 0.29179E+01
   Friction thermal sca.    tstar :  0.12103E+01 0.23893E+03
   Rough dim-less th. sca.  tplus :  0.52036E-02 0.20670E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26844E+00      11   0.16782E-04   0.59038E+01 0.38778E+02 
c  Velocity[X]                                      0.25738E+01 
c  Velocity[Y]                                      0.15420E+01 
c  Velocity[Z]                                      0.17880E+01 
c  Pressure     0.18887E-04      18   0.36627E-03   0.19775E-01 0.14281E+02 
c  k            0.21190E-01      13   0.67191E-04   0.19619E+00 0.59145E+02 
c  omega        0.27922E+07       1   0.10307E-06   0.12579E+08 0.64938E+00 
c  TempK        0.10054E+05       4   0.46068E-05   0.55457E+01 0.82647E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3579e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.248          19.147       0.0093503      -0.0093134
v  Velocity[Y]             -15.928           15.49         0.36968         0.54816
v  Velocity[Z]              -25.43          11.615         -1.6433        -0.50726
v  ǁVelocityǁ         0.00030007          25.816          7.6119          6.5066
v  Pressure                -520.07          172.31         -2.4617          3.0885
v  k                   9.7296e-011          6.5493         0.25754          0.5548
v  omega                    57.497     2.7317e+008     1.2912e+006           76835
v  TempK                    298.56          363.17          338.49          347.83
v  TurbVisc            2.4381e-018       0.0020536     6.6333e-005      0.00023263
v  CourantNb            0.00014031          1.5728         0.78809         0.96981
v  FourierNb             0.0037885               1         0.42474          0.1945
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0036487     7.4288e-005      0.00020256

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.57          306.64
v  Yplus               0          2.9179         0.62744         0.48187


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52155          2.1814          1.2128          1.1643


 INSTANT    0.101000000E-01   TIME STEP NUMBER            1010
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923952E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10858E-01 0.46905E+01
   Friction velocity        uk    :  0.10858E-01 0.46865E+01
   Dimensionless distance   yplus :  0.73617E-02 0.29179E+01
   Friction thermal sca.    tstar :  0.12105E+01 0.23840E+03
   Rough dim-less th. sca.  tplus :  0.52151E-02 0.20670E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26844E+00      11   0.16778E-04   0.59226E+01 0.38819E+02 
c  Velocity[X]                                      0.25806E+01 
c  Velocity[Y]                                      0.15425E+01 
c  Velocity[Z]                                      0.17996E+01 
c  Pressure     0.19017E-04      18   0.36578E-03   0.19914E-01 0.14328E+02 
c  k            0.21190E-01      13   0.66678E-04   0.19535E+00 0.58997E+02 
c  omega        0.27922E+07       1   0.10508E-06   0.18347E+08 0.73061E+00 
c  TempK        0.10055E+05       4   0.46052E-05   0.55567E+01 0.82731E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3515e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.249          19.147       0.0094958      -0.0092067
v  Velocity[Y]             -16.005          15.497         0.37027         0.54903
v  Velocity[Z]             -25.433          11.613         -1.6433         -0.5073
v  ǁVelocityǁ         0.00034692          25.819           7.612          6.5068
v  Pressure                -519.29          172.35         -2.4267          3.1209
v  k                   9.7297e-011          6.5597         0.25754         0.55477
v  omega                    57.497     2.7317e+008     1.2912e+006           76835
v  TempK                    298.56          363.17          338.49          347.84
v  TurbVisc            2.4381e-018       0.0020556     6.6329e-005      0.00023264
v  CourantNb             0.0001888          1.5744          0.7881         0.96982
v  FourierNb             0.0037885               1         0.42472         0.19446
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0035226     7.4283e-005      0.00020255

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.57          306.64
v  Yplus               0          2.9179         0.62745         0.48186


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46796           2.183          1.2128          1.1643


 INSTANT    0.101100000E-01   TIME STEP NUMBER            1011
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923989E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10857E-01 0.46905E+01
   Friction velocity        uk    :  0.10857E-01 0.46865E+01
   Dimensionless distance   yplus :  0.73609E-02 0.29179E+01
   Friction thermal sca.    tstar :  0.12110E+01 0.23843E+03
   Rough dim-less th. sca.  tplus :  0.52145E-02 0.20670E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26844E+00      11   0.16745E-04   0.59433E+01 0.38889E+02 
c  Velocity[X]                                      0.25867E+01 
c  Velocity[Y]                                      0.15484E+01 
c  Velocity[Z]                                      0.18082E+01 
c  Pressure     0.18972E-04      18   0.36208E-03   0.19870E-01 0.14289E+02 
c  k            0.21191E-01      13   0.65826E-04   0.19452E+00 0.58853E+02 
c  omega        0.27922E+07       1   0.10680E-06   0.24650E+08 0.81529E+00 
c  TempK        0.10055E+05       4   0.46028E-05   0.55620E+01 0.82781E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3458e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.249          19.147       0.0096435      -0.0090995
v  Velocity[Y]             -15.974          15.504         0.37086          0.5499
v  Velocity[Z]             -25.435          12.134         -1.6433        -0.50734
v  ǁVelocityǁ         0.00039405          25.821           7.612          6.5069
v  Pressure                -519.21          172.39         -2.3938          3.1512
v  k                   9.7297e-011          6.5687         0.25755         0.55474
v  omega                    57.497     2.7317e+008     1.2912e+006           76835
v  TempK                    298.57          363.17          338.49          347.84
v  TurbVisc            2.4381e-018       0.0020576     6.6325e-005      0.00023264
v  CourantNb            0.00020283          1.5758         0.78811         0.96982
v  FourierNb             0.0037885               1         0.42471         0.19442
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006        0.003508     7.4279e-005      0.00020254

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.57          306.64
v  Yplus               0          2.9179         0.62747         0.48185


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47776          2.1844          1.2128          1.1642


 INSTANT    0.101200000E-01   TIME STEP NUMBER            1012
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924028E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10930E-01 0.46904E+01
   Friction velocity        uk    :  0.10930E-01 0.46864E+01
   Dimensionless distance   yplus :  0.74106E-02 0.29179E+01
   Friction thermal sca.    tstar :  0.12111E+01 0.23683E+03
   Rough dim-less th. sca.  tplus :  0.52497E-02 0.20671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26843E+00      11   0.16672E-04   0.59561E+01 0.38882E+02 
c  Velocity[X]                                      0.25940E+01 
c  Velocity[Y]                                      0.15457E+01 
c  Velocity[Z]                                      0.18164E+01 
c  Pressure     0.18845E-04      17   0.36487E-03   0.19739E-01 0.13523E+02 
c  k            0.21191E-01      13   0.65709E-04   0.19381E+00 0.58707E+02 
c  omega        0.27922E+07       1   0.10420E-06   0.17784E+08 0.71132E+00 
c  TempK        0.10055E+05       4   0.45996E-05   0.55661E+01 0.82826E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3404e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.25          19.147       0.0097957      -0.0089943
v  Velocity[Y]             -15.877          15.511         0.37146         0.55078
v  Velocity[Z]             -25.438          12.502         -1.6433        -0.50736
v  ǁVelocityǁ         0.00039364          25.823          7.6121          6.5071
v  Pressure                -519.67          172.42         -2.3715          3.1717
v  k                   9.7297e-011          6.5764         0.25755         0.55471
v  omega                    57.497     2.7317e+008     1.2912e+006           76835
v  TempK                    298.57          363.17           338.5          347.85
v  TurbVisc            2.4381e-018       0.0020597     6.6321e-005      0.00023264
v  CourantNb            0.00024235          1.5772         0.78812         0.96983
v  FourierNb             0.0037886               1         0.42469         0.19438
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0036538     7.4275e-005      0.00020253

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.57          306.64
v  Yplus               0          2.9179         0.62748         0.48184


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61206          2.1857          1.2128          1.1642


 INSTANT    0.101300000E-01   TIME STEP NUMBER            1013
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923970E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10920E-01 0.46903E+01
   Friction velocity        uk    :  0.10920E-01 0.46863E+01
   Dimensionless distance   yplus :  0.74040E-02 0.29179E+01
   Friction thermal sca.    tstar :  0.12106E+01 0.23704E+03
   Rough dim-less th. sca.  tplus :  0.52450E-02 0.20671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         55 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26843E+00      11   0.16662E-04   0.59688E+01 0.38873E+02 
c  Velocity[X]                                      0.26006E+01 
c  Velocity[Y]                                      0.15431E+01 
c  Velocity[Z]                                      0.18251E+01 
c  Pressure     0.18679E-04      18   0.36595E-03   0.19567E-01 0.13550E+02 
c  k            0.21192E-01      13   0.65212E-04   0.19323E+00 0.58571E+02 
c  omega        0.27922E+07       1   0.10397E-06   0.18951E+08 0.72652E+00 
c  TempK        0.10055E+05       4   0.45968E-05   0.55726E+01 0.82870E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3348e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.251          19.147       0.0099503      -0.0088896
v  Velocity[Y]              -15.85          15.518         0.37206         0.55166
v  Velocity[Z]             -25.441          12.797         -1.6433        -0.50739
v  ǁVelocityǁ         0.00037818          25.826          7.6122          6.5073
v  Pressure                -520.09          172.45         -2.3458          3.1953
v  k                   9.7297e-011          6.5829         0.25756         0.55467
v  omega                    57.497     2.7317e+008     1.2912e+006           76835
v  TempK                    298.57          363.17           338.5          347.85
v  TurbVisc            2.4381e-018       0.0020617     6.6316e-005      0.00023265
v  CourantNb            0.00020012          1.5786         0.78813         0.96984
v  FourierNb             0.0037886               1         0.42467         0.19434
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0036048     7.4272e-005      0.00020252

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.57          306.64
v  Yplus               0          2.9179         0.62749         0.48184


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55767          2.1871          1.2128          1.1642


 INSTANT    0.101400000E-01   TIME STEP NUMBER            1014
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923979E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10931E-01 0.46903E+01
   Friction velocity        uk    :  0.10931E-01 0.46863E+01
   Dimensionless distance   yplus :  0.74113E-02 0.29179E+01
   Friction thermal sca.    tstar :  0.12109E+01 0.23681E+03
   Rough dim-less th. sca.  tplus :  0.52502E-02 0.20671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         55 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26843E+00      11   0.16686E-04   0.59847E+01 0.38880E+02 
c  Velocity[X]                                      0.26080E+01 
c  Velocity[Y]                                      0.15417E+01 
c  Velocity[Z]                                      0.18350E+01 
c  Pressure     0.18856E-04      18   0.37043E-03   0.19754E-01 0.13677E+02 
c  k            0.21191E-01      13   0.64799E-04   0.19267E+00 0.58432E+02 
c  omega        0.27922E+07       1   0.10126E-06   0.98862E+07 0.56642E+00 
c  TempK        0.10055E+05       4   0.45932E-05   0.55808E+01 0.82945E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3289e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.251          19.147        0.010107      -0.0087874
v  Velocity[Y]             -15.881          15.526         0.37266         0.55255
v  Velocity[Z]             -25.443           13.54         -1.6433        -0.50743
v  ǁVelocityǁ         0.00036838          25.828          7.6123          6.5074
v  Pressure                -520.37          172.48         -2.3174          3.2217
v  k                   9.7298e-011          6.5881         0.25755         0.55463
v  omega                    57.498     2.7317e+008     1.2912e+006           76835
v  TempK                    298.58          363.17           338.5          347.86
v  TurbVisc            2.4381e-018       0.0020636     6.6311e-005      0.00023265
v  CourantNb            0.00019195          1.5801         0.78814         0.96985
v  FourierNb             0.0037886               1         0.42464          0.1943
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0035517     7.4268e-005      0.00020251

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.57          306.64
v  Yplus               0          2.9179          0.6275         0.48183


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53879          2.1885          1.2128          1.1641


 INSTANT    0.101500000E-01   TIME STEP NUMBER            1015
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924005E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10935E-01 0.46902E+01
   Friction velocity        uk    :  0.10935E-01 0.46862E+01
   Dimensionless distance   yplus :  0.74143E-02 0.29179E+01
   Friction thermal sca.    tstar :  0.12110E+01 0.23671E+03
   Rough dim-less th. sca.  tplus :  0.52523E-02 0.20671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26842E+00      11   0.16722E-04   0.60068E+01 0.38924E+02 
c  Velocity[X]                                      0.26139E+01 
c  Velocity[Y]                                      0.15439E+01 
c  Velocity[Z]                                      0.18489E+01 
c  Pressure     0.19316E-04      18   0.37648E-03   0.20237E-01 0.14259E+02 
c  k            0.21191E-01      13   0.64475E-04   0.19218E+00 0.58308E+02 
c  omega        0.27922E+07       1   0.10482E-06   0.18292E+08 0.70602E+00 
c  TempK        0.10055E+05       4   0.45895E-05   0.55942E+01 0.83046E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3227e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.252          19.147        0.010264      -0.0086889
v  Velocity[Y]             -16.014          15.532         0.37325         0.55344
v  Velocity[Z]             -25.446          14.435         -1.6432        -0.50747
v  ǁVelocityǁ         0.00036486           25.83          7.6123          6.5076
v  Pressure                -519.82          172.53         -2.2825          3.2542
v  k                   9.7298e-011          6.5922         0.25755         0.55459
v  omega                    57.498     2.7317e+008     1.2912e+006           76835
v  TempK                    298.58          363.17          338.51          347.86
v  TurbVisc            2.4381e-018       0.0020656     6.6305e-005      0.00023265
v  CourantNb            0.00019902          1.5816         0.78815         0.96986
v  FourierNb             0.0037887               1         0.42462         0.19425
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034959     7.4265e-005       0.0002025

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.57          306.64
v  Yplus               0          2.9179         0.62751         0.48183


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53415            2.19          1.2128          1.1641


 INSTANT    0.101600000E-01   TIME STEP NUMBER            1016
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923887E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10963E-01 0.46902E+01
   Friction velocity        uk    :  0.10963E-01 0.46862E+01
   Dimensionless distance   yplus :  0.74332E-02 0.29179E+01
   Friction thermal sca.    tstar :  0.12114E+01 0.23611E+03
   Rough dim-less th. sca.  tplus :  0.52657E-02 0.20671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26842E+00      11   0.16713E-04   0.60368E+01 0.39005E+02 
c  Velocity[X]                                      0.26236E+01 
c  Velocity[Y]                                      0.15539E+01 
c  Velocity[Z]                                      0.18593E+01 
c  Pressure     0.19663E-04      18   0.38017E-03   0.20601E-01 0.14533E+02 
c  k            0.21190E-01      13   0.64515E-04   0.19184E+00 0.58220E+02 
c  omega        0.27922E+07       1   0.10208E-06   0.11596E+08 0.59212E+00 
c  TempK        0.10055E+05       4   0.45856E-05   0.56034E+01 0.83093E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3171e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.253          19.148         0.01042      -0.0085929
v  Velocity[Y]             -16.005          15.539         0.37385         0.55433
v  Velocity[Z]             -25.448          14.069         -1.6432        -0.50751
v  ǁVelocityǁ         0.00036759          25.833          7.6124          6.5077
v  Pressure                -519.07          172.57         -2.2434          3.2907
v  k                   9.7298e-011          6.5952         0.25755         0.55454
v  omega                    57.498     2.7317e+008     1.2912e+006           76835
v  TempK                    298.59          363.17          338.51          347.87
v  TurbVisc            2.4381e-018       0.0020676     6.6298e-005      0.00023265
v  CourantNb             0.0002067           1.583         0.78816         0.96988
v  FourierNb             0.0037887               1          0.4246         0.19421
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034301     7.4261e-005      0.00020249

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.57          306.64
v  Yplus               0          2.9179         0.62753         0.48182


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50648          2.1914          1.2128          1.1641


 INSTANT    0.101700000E-01   TIME STEP NUMBER            1017
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924036E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10954E-01 0.46901E+01
   Friction velocity        uk    :  0.10954E-01 0.46861E+01
   Dimensionless distance   yplus :  0.74270E-02 0.29179E+01
   Friction thermal sca.    tstar :  0.12113E+01 0.23631E+03
   Rough dim-less th. sca.  tplus :  0.52613E-02 0.20671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26842E+00      11   0.16770E-04   0.60615E+01 0.39039E+02 
c  Velocity[X]                                      0.26320E+01 
c  Velocity[Y]                                      0.15567E+01 
c  Velocity[Z]                                      0.18728E+01 
c  Pressure     0.19487E-04      18   0.38403E-03   0.20417E-01 0.13930E+02 
c  k            0.21189E-01      13   0.64156E-04   0.19149E+00 0.58150E+02 
c  omega        0.27922E+07       1   0.10516E-06   0.19805E+08 0.72892E+00 
c  TempK        0.10056E+05       4   0.45814E-05   0.56115E+01 0.83145E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3118e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.254          19.148        0.010577      -0.0084947
v  Velocity[Y]             -15.935          15.546         0.37445         0.55523
v  Velocity[Z]             -25.451          11.753         -1.6432        -0.50754
v  ǁVelocityǁ         0.00037649          25.835          7.6125          6.5079
v  Pressure                -519.68          172.61         -2.2148          3.3171
v  k                   9.7297e-011          6.5971         0.25754         0.55449
v  omega                    57.498     2.7317e+008     1.2912e+006           76835
v  TempK                     298.6          363.17          338.51          347.87
v  TurbVisc            2.4381e-018       0.0020695     6.6292e-005      0.00023265
v  CourantNb             0.0002159          1.5843         0.78817         0.96989
v  FourierNb             0.0037888               1         0.42457         0.19416
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034183     7.4258e-005      0.00020247

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.57          306.64
v  Yplus               0          2.9179         0.62754         0.48182


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49301          2.1926          1.2127          1.1641


 INSTANT    0.101800000E-01   TIME STEP NUMBER            1018
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923983E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11003E-01 0.46901E+01
   Friction velocity        uk    :  0.11003E-01 0.46861E+01
   Dimensionless distance   yplus :  0.74604E-02 0.29179E+01
   Friction thermal sca.    tstar :  0.12112E+01 0.23525E+03
   Rough dim-less th. sca.  tplus :  0.52850E-02 0.20671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26841E+00      11   0.17138E-04   0.60817E+01 0.39067E+02 
c  Velocity[X]                                      0.26341E+01 
c  Velocity[Y]                                      0.15641E+01 
c  Velocity[Z]                                      0.18835E+01 
c  Pressure     0.19282E-04      17   0.38619E-03   0.20202E-01 0.14676E+02 
c  k            0.21188E-01      13   0.63488E-04   0.19134E+00 0.58103E+02 
c  omega        0.27922E+07       1   0.10401E-06   0.15981E+08 0.66904E+00 
c  TempK        0.10056E+05       4   0.45773E-05   0.56201E+01 0.83181E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3067e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.255          19.148        0.010731      -0.0083972
v  Velocity[Y]             -15.888          15.553         0.37506         0.55613
v  Velocity[Z]             -25.453          11.603         -1.6432        -0.50757
v  ǁVelocityǁ         0.00039141          25.837          7.6126          6.5081
v  Pressure                -520.09          172.66         -2.1779          3.3512
v  k                   9.7297e-011          6.5981         0.25753         0.55444
v  omega                    57.498     2.7317e+008     1.2912e+006           76835
v  TempK                     298.6          363.17          338.52          347.88
v  TurbVisc            2.4381e-018       0.0020715     6.6286e-005      0.00023266
v  CourantNb            0.00023023          1.5856         0.78818         0.96991
v  FourierNb             0.0037888               1         0.42455         0.19412
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034463     7.4255e-005      0.00020246

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.57          306.64
v  Yplus               0          2.9179         0.62756         0.48182


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.31889          2.1939          1.2127           1.164


 INSTANT    0.101900000E-01   TIME STEP NUMBER            1019
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924061E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11043E-01 0.46900E+01
   Friction velocity        uk    :  0.11043E-01 0.46860E+01
   Dimensionless distance   yplus :  0.74875E-02 0.29180E+01
   Friction thermal sca.    tstar :  0.12113E+01 0.23440E+03
   Rough dim-less th. sca.  tplus :  0.53042E-02 0.20671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26841E+00      11   0.17244E-04   0.60971E+01 0.39077E+02 
c  Velocity[X]                                      0.26379E+01 
c  Velocity[Y]                                      0.15678E+01 
c  Velocity[Z]                                      0.18915E+01 
c  Pressure     0.19363E-04      18   0.39022E-03   0.20286E-01 0.13755E+02 
c  k            0.21187E-01      13   0.64350E-04   0.19164E+00 0.58088E+02 
c  omega        0.27922E+07       1   0.10324E-06   0.13996E+08 0.63724E+00 
c  TempK        0.10056E+05       4   0.45733E-05   0.56223E+01 0.83185E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.3012e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.256          19.148        0.010883      -0.0083011
v  Velocity[Y]             -15.879          15.559         0.37566         0.55704
v  Velocity[Z]             -25.456          11.601         -1.6432         -0.5076
v  ǁVelocityǁ         0.00041111          25.839          7.6127          6.5082
v  Pressure                -520.39          172.69         -2.1502          3.3764
v  k                   9.7297e-011           6.598         0.25752         0.55438
v  omega                    57.498     2.7317e+008     1.2912e+006           76835
v  TempK                    298.61          363.17          338.52          347.88
v  TurbVisc            2.4381e-018       0.0020734      6.628e-005      0.00023267
v  CourantNb            0.00024333           1.587          0.7882         0.96993
v  FourierNb             0.0037888               1         0.42452         0.19408
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034724     7.4253e-005      0.00020245

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.57          306.64
v  Yplus               0           2.918         0.62757         0.48182


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35221          2.1952          1.2127           1.164


 INSTANT    0.102000000E-01   TIME STEP NUMBER            1020
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923942E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11059E-01 0.46900E+01
   Friction velocity        uk    :  0.11059E-01 0.46860E+01
   Dimensionless distance   yplus :  0.74982E-02 0.29180E+01
   Friction thermal sca.    tstar :  0.12114E+01 0.23406E+03
   Rough dim-less th. sca.  tplus :  0.53118E-02 0.20671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26841E+00      11   0.17197E-04   0.61131E+01 0.39081E+02 
c  Velocity[X]                                      0.26395E+01 
c  Velocity[Y]                                      0.15701E+01 
c  Velocity[Z]                                      0.19035E+01 
c  Pressure     0.19312E-04      18   0.39271E-03   0.20232E-01 0.14291E+02 
c  k            0.21185E-01      13   0.64265E-04   0.19188E+00 0.58097E+02 
c  omega        0.27922E+07       1   0.10317E-06   0.13938E+08 0.63799E+00 
c  TempK        0.10056E+05       4   0.45701E-05   0.56224E+01 0.83190E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.2953e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.257          19.148        0.011035      -0.0082053
v  Velocity[Y]             -15.911          15.566         0.37627         0.55795
v  Velocity[Z]             -25.458            11.6         -1.6431        -0.50764
v  ǁVelocityǁ         0.00041777          25.841          7.6128          6.5084
v  Pressure                -520.53          172.74         -2.1126          3.4116
v  k                   9.7296e-011           6.597         0.25751         0.55431
v  omega                    57.498     2.7317e+008     1.2912e+006           76835
v  TempK                    298.62          363.17          338.52          347.89
v  TurbVisc            2.4381e-018       0.0020752     6.6275e-005      0.00023268
v  CourantNb            0.00024333          1.5885         0.78821         0.96995
v  FourierNb             0.0037889               1          0.4245         0.19404
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034951      7.425e-005      0.00020244

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.57          306.64
v  Yplus               0           2.918         0.62758         0.48182


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42421          2.1966          1.2127           1.164


 INSTANT    0.102100000E-01   TIME STEP NUMBER            1021
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924083E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11052E-01 0.46900E+01
   Friction velocity        uk    :  0.11052E-01 0.46860E+01
   Dimensionless distance   yplus :  0.74934E-02 0.29180E+01
   Friction thermal sca.    tstar :  0.12115E+01 0.23421E+03
   Rough dim-less th. sca.  tplus :  0.53084E-02 0.20671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26841E+00      11   0.17018E-04   0.61344E+01 0.39125E+02 
c  Velocity[X]                                      0.26442E+01 
c  Velocity[Y]                                      0.15771E+01 
c  Velocity[Z]                                      0.19132E+01 
c  Pressure     0.19496E-04      18   0.39694E-03   0.20425E-01 0.14446E+02 
c  k            0.21183E-01      13   0.63832E-04   0.19227E+00 0.58144E+02 
c  omega        0.27922E+07       1   0.10454E-06   0.16422E+08 0.67795E+00 
c  TempK        0.10056E+05       4   0.45679E-05   0.56248E+01 0.83202E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.2893e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.258          19.148        0.011187      -0.0081111
v  Velocity[Y]             -16.054          15.572         0.37687         0.55887
v  Velocity[Z]              -25.46          11.598         -1.6431        -0.50767
v  ǁVelocityǁ         0.00041757          25.843          7.6129          6.5086
v  Pressure                -519.47          172.78         -2.0762          3.4449
v  k                   9.7296e-011           6.595         0.25749         0.55425
v  omega                    57.498     2.7317e+008     1.2912e+006           76835
v  TempK                    298.63          363.17          338.52          347.89
v  TurbVisc            2.4381e-018        0.002077     6.6269e-005      0.00023268
v  CourantNb            0.00022324            1.59         0.78823         0.96997
v  FourierNb              0.003789               1         0.42448           0.194
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0035126     7.4247e-005      0.00020242

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.57          306.64
v  Yplus               0           2.918          0.6276         0.48183


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38641          2.1981          1.2127           1.164


 INSTANT    0.102200000E-01   TIME STEP NUMBER            1022
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923955E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11089E-01 0.46899E+01
   Friction velocity        uk    :  0.11089E-01 0.46859E+01
   Dimensionless distance   yplus :  0.75184E-02 0.29180E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.23343E+03
   Rough dim-less th. sca.  tplus :  0.53261E-02 0.20671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26840E+00      11   0.17083E-04   0.61530E+01 0.39178E+02 
c  Velocity[X]                                      0.26464E+01 
c  Velocity[Y]                                      0.15882E+01 
c  Velocity[Z]                                      0.19184E+01 
c  Pressure     0.19367E-04      18   0.40140E-03   0.20289E-01 0.14832E+02 
c  k            0.21180E-01      13   0.64139E-04   0.19268E+00 0.58217E+02 
c  omega        0.27922E+07       1   0.10499E-06   0.19510E+08 0.72892E+00 
c  TempK        0.10056E+05       4   0.45657E-05   0.56253E+01 0.83175E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.2842e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.259          19.149        0.011337      -0.0080181
v  Velocity[Y]             -15.976          15.579         0.37748         0.55978
v  Velocity[Z]             -25.463          11.597         -1.6431        -0.50769
v  ǁVelocityǁ         0.00041757          25.845           7.613          6.5087
v  Pressure                -519.48          172.83         -2.0331          3.4853
v  k                   9.7295e-011           6.592         0.25748         0.55418
v  omega                    57.498     2.7317e+008     1.2912e+006           76835
v  TempK                    298.63          363.17          338.53           347.9
v  TurbVisc            2.4381e-018       0.0020787     6.6263e-005      0.00023268
v  CourantNb            0.00018083          1.5913         0.78824         0.96998
v  FourierNb             0.0037891               1         0.42446         0.19395
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0035235     7.4243e-005      0.00020241

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.57          306.64
v  Yplus               0           2.918         0.62761         0.48183


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45017          2.1993          1.2127          1.1639


 INSTANT    0.102300000E-01   TIME STEP NUMBER            1023
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923989E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11086E-01 0.46899E+01
   Friction velocity        uk    :  0.11086E-01 0.46859E+01
   Dimensionless distance   yplus :  0.75162E-02 0.29180E+01
   Friction thermal sca.    tstar :  0.12116E+01 0.23350E+03
   Rough dim-less th. sca.  tplus :  0.53245E-02 0.20671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         55 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26840E+00      11   0.17184E-04   0.61614E+01 0.39143E+02 
c  Velocity[X]                                      0.26480E+01 
c  Velocity[Y]                                      0.15883E+01 
c  Velocity[Z]                                      0.19251E+01 
c  Pressure     0.19382E-04      17   0.39570E-03   0.20305E-01 0.14343E+02 
c  k            0.21177E-01      13   0.64394E-04   0.19324E+00 0.58306E+02 
c  omega        0.27922E+07       1   0.10327E-06   0.14506E+08 0.64762E+00 
c  TempK        0.10057E+05       4   0.45645E-05   0.56268E+01 0.83149E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.2793e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.26          19.149        0.011484      -0.0079224
v  Velocity[Y]               -15.9          15.585         0.37809         0.56071
v  Velocity[Z]             -25.465          11.595         -1.6431        -0.50771
v  ǁVelocityǁ         0.00041739          25.847          7.6131          6.5089
v  Pressure                -520.07          172.88         -1.9972          3.5189
v  k                   9.7294e-011          6.5881         0.25746         0.55411
v  omega                    57.498     2.7316e+008     1.2912e+006           76835
v  TempK                    298.63          363.17          338.53           347.9
v  TurbVisc            2.4381e-018       0.0020803     6.6256e-005      0.00023268
v  CourantNb             0.0002151          1.5925         0.78825            0.97
v  FourierNb             0.0037892               1         0.42443          0.1939
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0035259     7.4238e-005      0.00020239

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.57          306.64
v  Yplus               0           2.918         0.62763         0.48184


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.3982          2.2005          1.2127          1.1639


 INSTANT    0.102400000E-01   TIME STEP NUMBER            1024
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923966E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11118E-01 0.46899E+01
   Friction velocity        uk    :  0.11118E-01 0.46859E+01
   Dimensionless distance   yplus :  0.75383E-02 0.29180E+01
   Friction thermal sca.    tstar :  0.12115E+01 0.23282E+03
   Rough dim-less th. sca.  tplus :  0.53402E-02 0.20672E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26840E+00      11   0.18055E-04   0.61807E+01 0.39177E+02 
c  Velocity[X]                                      0.26503E+01 
c  Velocity[Y]                                      0.15930E+01 
c  Velocity[Z]                                      0.19373E+01 
c  Pressure     0.19133E-04      17   0.39948E-03   0.20044E-01 0.14791E+02 
c  k            0.21174E-01      13   0.64344E-04   0.19386E+00 0.58408E+02 
c  omega        0.27922E+07       1   0.10263E-06   0.12322E+08 0.60663E+00 
c  TempK        0.10057E+05       4   0.45632E-05   0.56295E+01 0.83120E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.274e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.261          19.149        0.011629      -0.0078262
v  Velocity[Y]             -15.872          15.592          0.3787         0.56163
v  Velocity[Z]             -25.467          12.143         -1.6431        -0.50773
v  ǁVelocityǁ         0.00040416          25.849          7.6133           6.509
v  Pressure                -520.41          172.93         -1.9555          3.5578
v  k                   9.7294e-011          6.5832         0.25745         0.55404
v  omega                    57.498     2.7316e+008     1.2912e+006           76835
v  TempK                    298.62          363.17          338.53          347.91
v  TurbVisc            2.4381e-018       0.0020817      6.625e-005      0.00023268
v  CourantNb            0.00024337          1.5939         0.78827         0.97001
v  FourierNb             0.0037893               1         0.42441         0.19386
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0036537     7.4234e-005      0.00020238

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.57          306.64
v  Yplus               0           2.918         0.62764         0.48185


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50285          2.2018          1.2127          1.1639


 INSTANT    0.102500000E-01   TIME STEP NUMBER            1025
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923975E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11164E-01 0.46899E+01
   Friction velocity        uk    :  0.11164E-01 0.46858E+01
   Dimensionless distance   yplus :  0.75692E-02 0.29180E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.23187E+03
   Rough dim-less th. sca.  tplus :  0.53621E-02 0.20672E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26840E+00      11   0.18042E-04   0.62033E+01 0.39234E+02 
c  Velocity[X]                                      0.26511E+01 
c  Velocity[Y]                                      0.16027E+01 
c  Velocity[Z]                                      0.19495E+01 
c  Pressure     0.19061E-04      17   0.40132E-03   0.19969E-01 0.14827E+02 
c  k            0.21170E-01      13   0.65243E-04   0.19488E+00 0.58544E+02 
c  omega        0.27922E+07       1   0.10589E-06   0.24263E+08 0.79683E+00 
c  TempK        0.10057E+05       4   0.45620E-05   0.56330E+01 0.83085E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.2685e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.262          19.149        0.011775        -0.00773
v  Velocity[Y]             -15.894          15.599         0.37931         0.56257
v  Velocity[Z]             -25.469          12.563          -1.643        -0.50775
v  ǁVelocityǁ          0.0003572          25.852          7.6134          6.5092
v  Pressure                -520.69          172.98         -1.9138          3.5966
v  k                   9.7293e-011           6.596         0.25743         0.55397
v  omega                    57.499     2.7316e+008     1.2912e+006           76835
v  TempK                    298.62          363.17          338.54          347.91
v  TurbVisc             2.438e-018        0.002083     6.6244e-005      0.00023269
v  CourantNb            0.00024338          1.5953         0.78828         0.97002
v  FourierNb             0.0037894               1         0.42439         0.19382
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0037034      7.423e-005      0.00020236

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.58          306.64
v  Yplus               0           2.918         0.62766         0.48186


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51453          2.2031          1.2127          1.1638


 INSTANT    0.102600000E-01   TIME STEP NUMBER            1026
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924018E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11217E-01 0.46898E+01
   Friction velocity        uk    :  0.11217E-01 0.46858E+01
   Dimensionless distance   yplus :  0.76052E-02 0.29181E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.23077E+03
   Rough dim-less th. sca.  tplus :  0.53876E-02 0.20672E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26840E+00      11   0.18287E-04   0.62182E+01 0.39221E+02 
c  Velocity[X]                                      0.26506E+01 
c  Velocity[Y]                                      0.16037E+01 
c  Velocity[Z]                                      0.19639E+01 
c  Pressure     0.19110E-04      17   0.40632E-03   0.20020E-01 0.14193E+02 
c  k            0.21167E-01      13   0.66039E-04   0.19608E+00 0.58698E+02 
c  omega        0.27922E+07       1   0.10651E-06   0.22322E+08 0.76371E+00 
c  TempK        0.10057E+05       4   0.45607E-05   0.56351E+01 0.83049E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.2627e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.263           19.15        0.011923      -0.0076301
v  Velocity[Y]             -15.981          15.605         0.37992          0.5635
v  Velocity[Z]             -25.472          12.665          -1.643        -0.50778
v  ǁVelocityǁ         0.00031122          25.854          7.6135          6.5093
v  Pressure                -520.57          173.02         -1.8781          3.6296
v  k                   9.7292e-011          6.6111         0.25741          0.5539
v  omega                    57.499     2.7316e+008     1.2912e+006           76835
v  TempK                    298.62          363.17          338.54          347.92
v  TurbVisc             2.438e-018       0.0020842     6.6239e-005       0.0002327
v  CourantNb             0.0002434          1.5968         0.78829         0.97003
v  FourierNb             0.0037895               1         0.42436         0.19378
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034687     7.4226e-005      0.00020235

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.58          306.64
v  Yplus               0          2.9181         0.62768         0.48188


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48628          2.2045          1.2127          1.1638


 INSTANT    0.102700000E-01   TIME STEP NUMBER            1027
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924018E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10779E-01 0.46898E+01
   Friction velocity        uk    :  0.10779E-01 0.46858E+01
   Dimensionless distance   yplus :  0.73081E-02 0.29181E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.23122E+03
   Rough dim-less th. sca.  tplus :  0.51771E-02 0.20672E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26840E+00      11   0.17979E-04   0.62475E+01 0.39269E+02 
c  Velocity[X]                                      0.26530E+01 
c  Velocity[Y]                                      0.16134E+01 
c  Velocity[Z]                                      0.19812E+01 
c  Pressure     0.19452E-04      17   0.40384E-03   0.20378E-01 0.14858E+02 
c  k            0.21162E-01      13   0.66698E-04   0.19751E+00 0.58877E+02 
c  omega        0.27922E+07       1   0.10266E-06   0.11903E+08 0.59375E+00 
c  TempK        0.10057E+05       4   0.45589E-05   0.56390E+01 0.82985E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.2572e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.264           19.15         0.01207      -0.0075285
v  Velocity[Y]             -16.049          15.611         0.38053         0.56443
v  Velocity[Z]             -25.474          11.818          -1.643        -0.50781
v  ǁVelocityǁ         0.00026471          25.855          7.6136          6.5095
v  Pressure                -519.69          173.08         -1.8364          3.6683
v  k                   9.7291e-011           6.619         0.25738         0.55382
v  omega                    57.499     2.7316e+008     1.2912e+006           76835
v  TempK                    298.62          363.17          338.54          347.92
v  TurbVisc             2.438e-018       0.0020862     6.6233e-005      0.00023271
v  CourantNb            0.00022328          1.5982          0.7883         0.97004
v  FourierNb             0.0037896               1         0.42434         0.19374
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0034285     7.4223e-005      0.00020235

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.58          306.64
v  Yplus               0          2.9181         0.62769         0.48189


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50892          2.2058          1.2126          1.1638


 INSTANT    0.102800000E-01   TIME STEP NUMBER            1028
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924039E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11228E-01 0.46898E+01
   Friction velocity        uk    :  0.11228E-01 0.46858E+01
   Dimensionless distance   yplus :  0.76128E-02 0.29181E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.23054E+03
   Rough dim-less th. sca.  tplus :  0.53929E-02 0.20672E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26839E+00      11   0.17558E-04   0.62775E+01 0.39302E+02 
c  Velocity[X]                                      0.26551E+01 
c  Velocity[Y]                                      0.16224E+01 
c  Velocity[Z]                                      0.20000E+01 
c  Pressure     0.19849E-04      18   0.41272E-03   0.20792E-01 0.14803E+02 
c  k            0.21157E-01      13   0.67621E-04   0.19906E+00 0.59090E+02 
c  omega        0.27922E+07       1   0.10245E-06   0.11466E+08 0.58842E+00 
c  TempK        0.10057E+05       4   0.45556E-05   0.56353E+01 0.82909E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.2521e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.264           19.15        0.012218      -0.0074287
v  Velocity[Y]             -15.991          15.617         0.38114         0.56537
v  Velocity[Z]             -25.476          11.586          -1.643        -0.50784
v  ǁVelocityǁ          0.0002189          25.857          7.6137          6.5096
v  Pressure                -519.69          173.13         -1.7953          3.7065
v  k                   9.7289e-011          6.6202         0.25736         0.55375
v  omega                    57.499     2.7316e+008     1.2912e+006           76835
v  TempK                    298.61          363.17          338.55          347.93
v  TurbVisc             2.438e-018       0.0020886     6.6226e-005      0.00023271
v  CourantNb            0.00022228          1.5995         0.78831         0.97005
v  FourierNb             0.0037897               1         0.42432         0.19371
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0033879     7.4221e-005      0.00020234

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.58          306.64
v  Yplus               0          2.9181          0.6277          0.4819


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43929          2.2071          1.2126          1.1638


 INSTANT    0.102900000E-01   TIME STEP NUMBER            1029
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924081E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11245E-01 0.46898E+01
   Friction velocity        uk    :  0.11245E-01 0.46858E+01
   Dimensionless distance   yplus :  0.76241E-02 0.29181E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.23020E+03
   Rough dim-less th. sca.  tplus :  0.54010E-02 0.20672E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26839E+00      11   0.17681E-04   0.62950E+01 0.39310E+02 
c  Velocity[X]                                      0.26535E+01 
c  Velocity[Y]                                      0.16290E+01 
c  Velocity[Z]                                      0.20125E+01 
c  Pressure     0.19556E-04      18   0.40655E-03   0.20485E-01 0.15058E+02 
c  k            0.21152E-01      13   0.67985E-04   0.20029E+00 0.59292E+02 
c  omega        0.27922E+07       1   0.10538E-06   0.21215E+08 0.74986E+00 
c  TempK        0.10058E+05       4   0.45517E-05   0.56246E+01 0.82782E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.2474e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.265          19.151        0.012365        -0.00733
v  Velocity[Y]             -15.894          15.624         0.38174         0.56631
v  Velocity[Z]             -25.478          11.584          -1.643        -0.50787
v  ǁVelocityǁ         0.00017556          25.859          7.6138          6.5098
v  Pressure                -520.15          173.18         -1.7507          3.7484
v  k                   9.7288e-011          6.6154         0.25733         0.55368
v  omega                    57.499     2.7316e+008     1.2912e+006           76835
v  TempK                    298.61          363.17          338.55          347.93
v  TurbVisc            2.4379e-018       0.0020907     6.6219e-005      0.00023272
v  CourantNb            0.00021145          1.6007         0.78832         0.97006
v  FourierNb             0.0037898               1         0.42431         0.19367
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006        0.003337     7.4219e-005      0.00020233

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.58          306.64
v  Yplus               0          2.9181         0.62772         0.48191


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45966          2.2082          1.2126          1.1637


 INSTANT    0.103000000E-01   TIME STEP NUMBER            1030
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924085E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11265E-01 0.46898E+01
   Friction velocity        uk    :  0.11265E-01 0.46858E+01
   Dimensionless distance   yplus :  0.76380E-02 0.29181E+01
   Friction thermal sca.    tstar :  0.12117E+01 0.22978E+03
   Rough dim-less th. sca.  tplus :  0.54108E-02 0.20672E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26839E+00      11   0.17832E-04   0.63182E+01 0.39331E+02 
c  Velocity[X]                                      0.26568E+01 
c  Velocity[Y]                                      0.16360E+01 
c  Velocity[Z]                                      0.20254E+01 
c  Pressure     0.19519E-04      18   0.41240E-03   0.20446E-01 0.14786E+02 
c  k            0.21146E-01      13   0.68247E-04   0.20184E+00 0.59523E+02 
c  omega        0.27922E+07       1   0.10271E-06   0.12162E+08 0.59898E+00 
c  TempK        0.10058E+05       4   0.45484E-05   0.56188E+01 0.82688E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.2425e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.266          19.151        0.012515      -0.0072307
v  Velocity[Y]             -15.836           15.63         0.38236         0.56726
v  Velocity[Z]              -25.48          11.582         -1.6429         -0.5079
v  ǁVelocityǁ         0.00013395          25.861           7.614          6.5099
v  Pressure                -520.54          173.23         -1.7098          3.7859
v  k                   9.7287e-011          6.6052         0.25731         0.55361
v  omega                    57.499     2.7316e+008     1.2912e+006           76835
v  TempK                    298.61          363.17          338.55          347.94
v  TurbVisc            2.4379e-018       0.0020885     6.6211e-005      0.00023273
v  CourantNb            0.00016489          1.6019         0.78833         0.97007
v  FourierNb               0.00379               1         0.42428         0.19364
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0033112     7.4217e-005      0.00020232

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.58          306.64
v  Yplus               0          2.9181         0.62773         0.48193


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42222          2.2094          1.2126          1.1637


 INSTANT    0.103100000E-01   TIME STEP NUMBER            1031
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923944E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11320E-01 0.46898E+01
   Friction velocity        uk    :  0.11320E-01 0.46858E+01
   Dimensionless distance   yplus :  0.76751E-02 0.29181E+01
   Friction thermal sca.    tstar :  0.12119E+01 0.22867E+03
   Rough dim-less th. sca.  tplus :  0.54371E-02 0.20672E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26839E+00      11   0.17965E-04   0.63376E+01 0.39373E+02 
c  Velocity[X]                                      0.26576E+01 
c  Velocity[Y]                                      0.16471E+01 
c  Velocity[Z]                                      0.20328E+01 
c  Pressure     0.19455E-04      18   0.41769E-03   0.20380E-01 0.15639E+02 
c  k            0.21140E-01      13   0.68890E-04   0.20355E+00 0.59773E+02 
c  omega        0.27922E+07       1   0.10553E-06   0.21746E+08 0.75781E+00 
c  TempK        0.10058E+05       4   0.45447E-05   0.56138E+01 0.82599E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.2371e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.267          19.152         0.01267      -0.0071303
v  Velocity[Y]              -15.84          15.636         0.38297         0.56821
v  Velocity[Z]             -25.482           11.58         -1.6429        -0.50791
v  ǁVelocityǁ        9.8324e-005          25.863          7.6141          6.5101
v  Pressure                -520.87           173.3         -1.6595          3.8328
v  k                   9.7285e-011          6.5906         0.25728         0.55355
v  omega                    57.499     2.7316e+008     1.2912e+006           76835
v  TempK                    298.61          363.17          338.55          347.94
v  TurbVisc            2.4379e-018       0.0020902     6.6204e-005      0.00023274
v  CourantNb             0.0002349          1.6033         0.78834         0.97008
v  FourierNb             0.0037901               1         0.42427          0.1936
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0033043     7.4216e-005      0.00020231

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.58          306.64
v  Yplus               0          2.9181         0.62774         0.48194


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40643          2.2106          1.2126          1.1637


 INSTANT    0.103200000E-01   TIME STEP NUMBER            1032
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924077E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94103E-02 0.46898E+01
   Friction velocity        uk    :  0.94103E-02 0.46857E+01
   Dimensionless distance   yplus :  0.63803E-02 0.29182E+01
   Friction thermal sca.    tstar :  0.12120E+01 0.27604E+03
   Rough dim-less th. sca.  tplus :  0.45199E-02 0.20672E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26839E+00      11   0.18165E-04   0.63519E+01 0.39341E+02 
c  Velocity[X]                                      0.26570E+01 
c  Velocity[Y]                                      0.16493E+01 
c  Velocity[Z]                                      0.20455E+01 
c  Pressure     0.19632E-04      18   0.41847E-03   0.20565E-01 0.14172E+02 
c  k            0.21133E-01      13   0.69848E-04   0.20549E+00 0.60051E+02 
c  omega        0.27922E+07       1   0.10444E-06   0.16483E+08 0.67429E+00 
c  TempK        0.10058E+05       4   0.45404E-05   0.56090E+01 0.82503E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.2314e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.268          19.152        0.012828      -0.0070249
v  Velocity[Y]             -15.883          15.643         0.38359         0.56916
v  Velocity[Z]             -25.484          12.381         -1.6429        -0.50793
v  ǁVelocityǁ        7.7816e-005          25.865          7.6142          6.5102
v  Pressure                -521.03          173.34         -1.6249          3.8641
v  k                   9.7284e-011          6.5721         0.25726         0.55349
v  omega                    57.499     2.7316e+008     1.2912e+006           76835
v  TempK                     298.6          363.17          338.56          347.94
v  TurbVisc            2.4378e-018       0.0020916     6.6197e-005      0.00023275
v  CourantNb            0.00024354          1.6048         0.78835         0.97009
v  FourierNb             0.0037902               1         0.42425         0.19357
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0032935     7.4214e-005       0.0002023

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.58          306.64
v  Yplus               0          2.9182         0.62776         0.48196


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44977           2.212          1.2126          1.1637


 INSTANT    0.103300000E-01   TIME STEP NUMBER            1033
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484923903E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44130E-02 0.46897E+01
   Friction velocity        uk    :  0.44130E-02 0.46857E+01
   Dimensionless distance   yplus :  0.29921E-02 0.29182E+01
   Friction thermal sca.    tstar :  0.12120E+01 0.58862E+03
   Rough dim-less th. sca.  tplus :  0.21196E-02 0.20673E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26839E+00      11   0.18281E-04   0.63746E+01 0.39359E+02 
c  Velocity[X]                                      0.26562E+01 
c  Velocity[Y]                                      0.16545E+01 
c  Velocity[Z]                                      0.20638E+01 
c  Pressure     0.19756E-04      18   0.41737E-03   0.20695E-01 0.15766E+02 
c  k            0.21127E-01      13   0.71165E-04   0.20769E+00 0.60350E+02 
c  omega        0.27922E+07       1   0.10561E-06   0.18439E+08 0.70256E+00 
c  TempK        0.10058E+05       4   0.45345E-05   0.56036E+01 0.82433E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.2256e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.268          19.152        0.012987       -0.006923
v  Velocity[Y]             -16.028          15.648          0.3842         0.57011
v  Velocity[Z]             -25.486          12.829         -1.6429        -0.50795
v  ǁVelocityǁ        8.3419e-005          25.867          7.6143          6.5103
v  Pressure                -519.99          173.41         -1.5742          3.9112
v  k                   9.7283e-011          6.5489         0.25723         0.55343
v  omega                      57.5     2.7316e+008     1.2912e+006           76835
v  TempK                     298.6          363.17          338.56          347.95
v  TurbVisc            2.4378e-018       0.0020927     6.6189e-005      0.00023276
v  CourantNb            0.00024357          1.6063         0.78836          0.9701
v  FourierNb             0.0037903               1         0.42423         0.19354
v  total_pressure      1.0081e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0032756     7.4211e-005      0.00020228

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.58          306.65
v  Yplus               0          2.9182         0.62777         0.48197


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44891          2.2134          1.2126          1.1636


 INSTANT    0.103400000E-01   TIME STEP NUMBER            1034
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924005E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71899E-02 0.46897E+01
   Friction velocity        uk    :  0.71899E-02 0.46857E+01
   Dimensionless distance   yplus :  0.48749E-02 0.29182E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.36128E+03
   Rough dim-less th. sca.  tplus :  0.34534E-02 0.20673E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26839E+00      11   0.18364E-04   0.64011E+01 0.39410E+02 
c  Velocity[X]                                      0.26560E+01 
c  Velocity[Y]                                      0.16686E+01 
c  Velocity[Z]                                      0.20765E+01 
c  Pressure     0.20088E-04      18   0.42041E-03   0.21043E-01 0.15228E+02 
c  k            0.21120E-01      13   0.72108E-04   0.20998E+00 0.60665E+02 
c  omega        0.27922E+07       1   0.10580E-06   0.20903E+08 0.74223E+00 
c  TempK        0.10058E+05       4   0.45286E-05   0.55860E+01 0.82301E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.2206e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.269          19.153        0.013147      -0.0068242
v  Velocity[Y]             -15.953          15.654         0.38481         0.57106
v  Velocity[Z]             -25.488          12.919         -1.6428        -0.50797
v  ǁVelocityǁ         0.00011127          25.868          7.6145          6.5105
v  Pressure                -520.01          173.47         -1.5288          3.9534
v  k                   9.7281e-011          6.5203          0.2572         0.55338
v  omega                      57.5     2.7316e+008     1.2912e+006           76835
v  TempK                     298.6          363.17          338.56          347.95
v  TurbVisc            2.4378e-018       0.0020934     6.6181e-005      0.00023277
v  CourantNb             0.0002436          1.6076         0.78836         0.97011
v  FourierNb             0.0037904               1         0.42421         0.19351
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0032514     7.4208e-005      0.00020227

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.58          306.65
v  Yplus               0          2.9182         0.62778         0.48198


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52185          2.2146          1.2126          1.1636


 INSTANT    0.103500000E-01   TIME STEP NUMBER            1035
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924059E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11014E-01 0.46897E+01
   Friction velocity        uk    :  0.11014E-01 0.46857E+01
   Dimensionless distance   yplus :  0.74678E-02 0.29182E+01
   Friction thermal sca.    tstar :  0.12119E+01 0.23583E+03
   Rough dim-less th. sca.  tplus :  0.52902E-02 0.20673E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26839E+00      11   0.18339E-04   0.64158E+01 0.39366E+02 
c  Velocity[X]                                      0.26573E+01 
c  Velocity[Y]                                      0.16702E+01 
c  Velocity[Z]                                      0.20883E+01 
c  Pressure     0.20603E-04      18   0.41975E-03   0.21583E-01 0.15264E+02 
c  k            0.21112E-01      13   0.73326E-04   0.21237E+00 0.60974E+02 
c  omega        0.27922E+07       1   0.10371E-06   0.14265E+08 0.63347E+00 
c  TempK        0.10059E+05       4   0.45222E-05   0.55674E+01 0.82177E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step      6.216e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.27          19.153        0.013309      -0.0067268
v  Velocity[Y]             -15.865          15.661         0.38543         0.57202
v  Velocity[Z]              -25.49           12.22         -1.6428        -0.50798
v  ǁVelocityǁ         0.00014934           25.87          7.6146          6.5106
v  Pressure                -520.67          173.52         -1.4835          3.9958
v  k                    9.728e-011          6.4878         0.25717         0.55332
v  omega                      57.5     2.7316e+008     1.2912e+006           76835
v  TempK                     298.6          363.17          338.57          347.96
v  TurbVisc            2.4377e-018       0.0020938     6.6173e-005      0.00023278
v  CourantNb            0.00018516          1.6088         0.78837         0.97012
v  FourierNb             0.0037905               1          0.4242         0.19348
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0032211     7.4205e-005      0.00020226

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.58          306.65
v  Yplus               0          2.9182         0.62779           0.482


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49603          2.2157          1.2126          1.1636


 INSTANT    0.103600000E-01   TIME STEP NUMBER            1036
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924051E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11443E-01 0.46897E+01
   Friction velocity        uk    :  0.11443E-01 0.46857E+01
   Dimensionless distance   yplus :  0.77583E-02 0.29183E+01
   Friction thermal sca.    tstar :  0.12118E+01 0.22622E+03
   Rough dim-less th. sca.  tplus :  0.54960E-02 0.20673E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       6290

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26839E+00      11   0.18916E-04   0.64393E+01 0.39387E+02 
c  Velocity[X]                                      0.26577E+01 
c  Velocity[Y]                                      0.16757E+01 
c  Velocity[Z]                                      0.21059E+01 
c  Pressure     0.21069E-04      17   0.42345E-03   0.22070E-01 0.15510E+02 
c  k            0.21105E-01      13   0.74213E-04   0.21477E+00 0.61290E+02 
c  omega        0.27922E+07       1   0.10275E-06   0.11249E+08 0.57546E+00 
c  TempK        0.10059E+05       4   0.45158E-05   0.55467E+01 0.82069E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.2109e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -18.27          19.154        0.013473      -0.0066315
v  Velocity[Y]             -15.829          15.667         0.38605         0.57298
v  Velocity[Z]             -25.492          11.569         -1.6428        -0.50799
v  ǁVelocityǁ         0.00019135          25.872          7.6147          6.5108
v  Pressure                -521.04          173.59         -1.4356          4.0406
v  k                   9.7278e-011          6.4522         0.25714         0.55327
v  omega                      57.5     2.7316e+008     1.2912e+006           76834
v  TempK                     298.6          363.17          338.57          347.96
v  TurbVisc            2.4377e-018       0.0020936     6.6164e-005       0.0002328
v  CourantNb             0.0002031          1.6101         0.78838         0.97014
v  FourierNb             0.0037906               1         0.42418         0.19345
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0031867     7.4201e-005      0.00020224

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.58          306.65
v  Yplus               0          2.9183          0.6278         0.48201


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47811          2.2169          1.2126          1.1636


 INSTANT    0.103700000E-01   TIME STEP NUMBER            1037
 ============================================================= 



 Options set or changed by "control_file":
 -------------------------

  max_time_step                            1037 (current: 1037)
   ignored control command: "?vq1"

 Finished reading "control_file".



   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       12644        -0.484924740E-01
Smooth wall               5      101444         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        3393         0.000000000E+00
Free outlet               3        6290         0.484924090E-01
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11475E-01 0.46898E+01
   Friction velocity        uk    :  0.11475E-01 0.46858E+01
   Dimensionless distance   yplus :  0.77800E-02 0.29183E+01
   Friction thermal sca.    tstar :  0.12120E+01 0.22559E+03
   Rough dim-less th. sca.  tplus :  0.55114E-02 0.20673E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :     101444
   Total number of wall faces                   :     101444
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       6290


 Write final restart files
   checkpoint at iteration       1037, Physical time    0.10370E-01


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint\main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint\main
 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                            
  Wrote boundary condition coefficients to checkpoint: checkpoint\auxiliary
   End writing the wall distance                        
 End writing

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.26839E+00      11   0.19466E-04   0.64585E+01 0.39428E+02 
c  Velocity[X]                                      0.26526E+01 
c  Velocity[Y]                                      0.16852E+01 
c  Velocity[Z]                                      0.21206E+01 
c  Pressure     0.21026E-04      18   0.42755E-03   0.22024E-01 0.15606E+02 
c  k            0.21096E-01      13   0.75582E-04   0.21767E+00 0.61644E+02 
c  omega        0.27922E+07       1   0.10456E-06   0.15836E+08 0.65684E+00 
c  TempK        0.10059E+05       4   0.45084E-05   0.55247E+01 0.81947E+00 
----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  TempK          
a  Local Time Step     6.2056e-007                             6


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -18.271          19.154        0.013638      -0.0065405
v  Velocity[Y]             -15.844          15.673         0.38669         0.57394
v  Velocity[Z]             -25.494          11.567         -1.6428          -0.508
v  ǁVelocityǁ         0.00023481          25.874          7.6149          6.5109
v  Pressure                -521.36          173.65         -1.3868          4.0854
v  k                   9.7276e-011          6.4183         0.25711         0.55323
v  omega                      57.5     2.7315e+008     1.2912e+006           76834
v  TempK                     298.6          363.17          338.57          347.97
v  TurbVisc            2.4376e-018        0.002093     6.6156e-005      0.00023282
v  CourantNb             0.0002376          1.6114         0.78839         0.97016
v  FourierNb             0.0037906               1         0.42416         0.19343
v  total_pressure       1.008e+005      1.015e+005     1.0132e+005     1.0133e+005
v  Local Time Step          1e-006       0.0031526     7.4196e-005      0.00020223

  ** Computed fields on boundary_faces
     ---------------------------------

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  TempK          298.15          363.17          305.58          306.65
v  Yplus               0          2.9183         0.62781         0.48203


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49501          2.2182          1.2126          1.1636



===============================================================



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


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                      END OF CALCULATION                     
                      ==================                     


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 Destroying structures and ending computation
